Preliminary Gemini 4 Crew Debriefing, Part II, 1965
NASA-UAP-D017 · Release 03 (6/12)
Agency
NASA
Document type
PDF
Location
North Atlantic Ocean (Other)
Incident date
6/9/65
Release
Release 03 (6/12)
Evidence tier
Tier 2 · Documented firsthand report
What the document says
This document is a preliminary transcript (Part II) derived from voice recordings of the Gemini 4 flight crew debriefing taken aboard the recovery ship, USS Wasp, on June 9, 1965. Part II of this document contains the “Visual Sightings” section of the debriefing (pages 196-224), where astronauts James McDivitt and Edward White describe their observations while aboard the spacecraft.
Auto-extracted from the original scan with OCR · may contain extraction artifacts. The source document above is authoritative.
DECLASSIFIED
Authority: 6 5
NW 91526
PRELIMINARY
GT-4 FLIGHT CREW DEBRIEFING TRANSCRIPT
PART II
Prepared By
Spacecraft Operations Branch
Flight Crew Support Division
June 18, 1965
This material contains information affecting the
national defense of the United States within the
meaning of the Espionage Laws, Title 18. U.S. C.
Section 793 and 794, the transmission or revela=
tion of which in any manner to an unauthorized
person is prohibited by law.
Group 4: Downgrade at 3 year intervals
Declassified after 12 years
NOTICE: This document may be exempt from
public disclosure under the Freedom of Infor-
mation Act (5 U.S.C, 552). Requests for its re-
lease to persons outside the U.S. Government
fm, should be handled under the provisions of
JERE NASA Policy Directive 1382.2.
PREFACE
This preliminary transcript was made from voice tape recordings
of the GT-4 flight crew debriefing conducted aboard the recovery ship,
the USS Wasp, on June 9, 1965, and concluded at the Manned Spacecraft
Center on June 12, 1965,
Although all the material contained in this transcript has been
edited, the urgent need for the preliminary transcript by mission
analysis personnel precluded a thorough editorial review prior to its
publication. Errors in this transcript will be corrected as soon as
possible and an official transcript will be published at a later date,
This document contains a transcript of the second part of the
total debriefing. A preliminary transcript of the first part was
published on June 16, 1965, and it contains the crew's description
of the mission from an operational standpoint.
GONARES TAPE
TABLE OF CONTENTS
Paragraph Page number
8.0
9.0
10.0
SYSTEMS OPERATION
8.1 Platform BRACELET ae aOR TTR Ae RINEE Rieiace rere Ave pene ee laueiace:areoeeretecereer Mere
OAMS Sac en mW AB Sy Se a i a wen SSE
RCS ace RAS ace eshte inveterate lei ellese ele céte:w olwleleveliela- ternal e eierece tatelncereta ene EE
Bnvironnental. Control SYSTEM eaiuie wei eis eeeea eee eee ere Kee
BONNET GATTOUA cecimetecnmcurareciees exeayadoluuemaem eee are Ge
BIGCULPICET SY SECM: eiseteseecwienwcere-wcesniy wresece: eye averwcee caja nieces Oe
COMPUEEST: susecerwaceierw ete eie cede acetetie casi sete Wim 6m iin la fanaa jaca te chicane ance tanalara AER
GREW GAEL ON iscnyesece cere ein ewer cere selene tea Ae a Sree eee SN eee TD
BE OS MGGE CAC. atecovereisieisseveeiee Mie SMS MCe[esE WON SHEIMLREM NICE eTRTepTRRSLatereceR ou
.
. * s
SO MJ OW Ww Po
OoOooomooooan
* «
OPERATIONAL CHECKS
Apollo Landmark Identification (D-6) .....cecceeeeeeeee 144
ADOLLG Yaw OP LSTGAREGN. ieargtedleweweaenws papers epeieewen TOO
One Attitude Thruster Failure Check ...-cesssessccveseel ll
Horizon Scanner Track Check) 4 wseceseswa ea eee sea eeees Le
Horigon: Scanner. CHE scawanawscqewes pesawe ewwewadeey 15
HF Transmission Reception Check ..scseeescseeccecreeees 181
Orbit Navigation Check wawsessawsewws oo oa ck ee ee eawae os 1B!
Relative Humldlty Vest isscnscnee ea wwwasa sein coe ee weed 1D
S00 acel Tight CHSCK asweeweeaneeew wera caeeen an ea en oe 186
ae)
*.
hm 09 SO @M 7 OW ew Pp =
ISUAL SIGHTINGS
SOOT OWED ance erwin pice ececatins a lar dametaciecierete aw aw aries pauiine ao aie era atarietalcaa
POWSPSH FIDE DG ape eicaiw eo ae eae ee eee eee once ace elects TOD
(OL) SOPODta L. PIE ERE ose ents ene wr Rac deee eee weeem ences wares HO
RO: RUE cet acces cea mcmama. ap rere te OR ARN Rn ee. ms RLS mi epNnie Race RTTa DOTS IE
ah nash,
oocs \O SO SO SO 80 50 40 80 40
*.
.
11.0 EXPERIMENTS
41.1 Two-Color Harth-Limb Photography (MSC-10) ......es-e0000217
11.2 Synoptic Terrain and Weather Photography (S-5 and S-6).219
11.3 Simple Navigation with the Sextant ...cccecssvnnvevenceald
11.4 Electrostatic Charge (MSC-1) ....-cceecececceceee cece e 229
11.5 Proton-Electron Spectrometer and Tri-Axis Flus-Gate
Magnetometer (MSC-2 and MSC=3) .....cccccccwcccnncsue ce 229
11.6 Radiation (D-8) ...... FG g Sied A nie on dik Mae ern ee ee
11.7 Inflight Exerciser (M-3) ....eccecccerccecveccsesceress230
11.8 Inflight Phonocardiogram (M-4) ......cceeeces ee hoe ee
‘tao’ xtrevehteular Activity: sscsniscned. cote saeneeeeurcew dese
l3)0: (Metecelteneous) 4 aw aiw nis eis acbsoin ei b/aie eine 010.0 a°9 a aioe ances dine asaece
TWORFRENTAL.
12,0 PRE-MISSION PLANNING
12.1 Mission Plan (Trajectory) ..ccceececerseaeeee ee 3
12.2 UL UA aces M a aicalay wre Messacatcasaneseiecmnermeans Sone eee Ga ce) Co 234
12.4 Spacecraft Changes ........ sonra ierae mca cere eters ecw aca ane ada nae one 239
1224 es OPS eS ae Mececareat actaresaeliasucaneneece ark eee cenemreruent eee 5 soe ee AO
12.5 Experiments .....0+5 PES NIRS AEBS EEC ET eo ee ee 244
12.6 Training Activities ...ses0e00es CET MO LOTT CREECH cha ee re 2A5
14.0 MISSION CONTROL
1334) COVNO GO" emende hens cowsnauns emda Aeneas es ion pA me 249
13.2 PLA and CLA Updates ......ceecees ee, 5...) a 249
1365 <GOVISUTHADLES aecew eases Fe ee ee 249
13.4 Flight Plan —— thc he MM die, ACL se A otinrge la RO en 250
TS eS =SYBTCHIB ere ecieie ee ececwte tna ie eanetn ener ARTES RETA RETICAL CORRE 254
14.0 TRAINING
1401 Gemini. Mission Sim1StOY coscwssawwceness ewe ewe ewe wes 255
122 TV Sa A TLOR J wassreeensterescdicanniw trans Ronnnsa eeeceiearesetvea ate ceod 260
1403 COPE PIEISE cdi aes ew cee aea rae arene nae ees 261
14.4 Transleticn atid Decking TPeine®” cscs wicewortae asowsaeesie® 262
1455 PISHbtarTum. sais ucwsas woes Seca ra ea tk aN LODGE NTA SOW DR WL OEE 263%
14.6 Syaetems BrISMss cacuvwwweweevenas Pe ee 266
We RISB BaperinieGntS! .ccaseeeue sew aw re ee ae 267
14.8 ppacecraft: Syabems TES? veces eae eau eee PTS
14.9 Egress Training ...... ena copearecernuane somimnsnunem te otrete sSiuedewrwerear 274
eI: PePRe MERE ASS x casceae Wie iete ee memes aire ie sanelnetera ie sgsiseiravie Tad ners 265
VAST eR Se BOR aoe re ontescenecenereecnvennuauececet ure ceecaseccec asa tevb rey 5: etcoea 276
14 et2: NEKO SAMOA ED OE cessor tess uence cececeyececerace aucun KPA ace erence 2EE
M.45 (ero NE BV eae cee momieve cece cwsay ee ie mana cece (eee ce la ete eee 18
T4<14. -ltehe Plan TEA eS opus deere ceca urwaaces OE cana neat acexesutacace ih
8.1 Platform
McDivitt
White
McDivitt
White
McDivitt
8.0 SYSTEMS OPERATION
Actually, the first portion of any alinement is
to cage the thing. The case of caging the thing
is much more important than the alinement itself.
In the daytime I felt that I could cage the plet-
form to a reference with an error plus or minus
about 3 or 4 degrees in all axes. Did you think
we could do that well?
Only in the daytime.
The yaw was a little problem. It took longer
to get it, but if you kept after it for awhile,
I felt that you could get down to just a few
degrees.
Within a couple of degrees.
The big thing is that you have to stop your yaw
rates, and then sit there and look outside for
awhile and see which way you're going, straight
ahead or sideways. If you are going sideways
you rotate around for awhile and stop the rate
and then lock out again. Right? I felt you could
get the thing caged quite well. We. didn't do it
BEF at all, did we? We never did cage in BHF.
”
White
McDivitt
White
McDivitt
I'm not sure.
The caging of the thing with small-end-forwerd in
the daytime was relatively easy. At night I don't
think it would be quite that simple. I think what
you would have to do at night time is to point
the spacecraft down at the ground pretty much so
you can see the track across the ground. I could
see which way the land was moving under me, If
felt--although I never did this--that if I could
do that and then roll around to where I had no
yank angle, and face in my yaw direction, either
small-end or blunt-end-forward, stop the roll there
and pitch up to the horizon I could cage there
within plus or minus 10 degrees for sure. It was
much less accurate at night, I felt, than in the
daytime.
You aren't kidding! We both felt that on those
dark nights when you really couldn't see anything
on the ground, pure star reference for yaw was
pretty rough.
Pure star reference for yaw was almost impossible
to use. That was the only place where that thing
we decided not to take with us--the view of the
stars through the window--might have been of some
TSSNADENTAL,....«
White
MeDivitt
use to us. We knew the stars along our track but
you couldn't see enough of them. The quickest
way to get the yaw reference was to look down at
the ground. Once we got the platform caged, aline-
ment was quite simple. All you had to do was just
hold the needles at zero and the platform alined
itself. Of course you had to have the scanners
on. The modes--the SHF and the BEF were identically
the same except the spacecraft is pointing in
different directions. You tended to null the
needles by using pulses and just hold the needles
very close to null and the platform alined itself
through the horizon scanners. Orbit Rate was a
satisfactory mode, I thought. As a matter of fact,
it was very good.
I liked that Orbit Rate.
Yes, because we finally had a reference where we
didn't have to look out and see the ground. It's
like having the old altitude indicator back in an
airplane. The only thing was, we had the wrong
orbit rate in the spacecraft because it was set
for an orbit rate that was to take care of, I
think, a 60 nautical mile circular orbit. This
was to take care of the short period of time between
White
McDivitt
werrpintaS”
going to Orbit Rate at T-5 and firing the retros
at TR, We wanted to have exactly the right rate
in there so when we did our closed-loop reentry
we wouldn't have an error. As I said, I had the
most accurate platform in the world with nothing
to do with it. I think the displays were adequate
and the controls were adequate. After the first
couple of revs I really didn't have any confidence
at all in the platform. I had done nothing to
establish any confidence in it. I really didn't
get the chance to get the thing alined, and I
really didn't have the view out the window to check
it with. We were hurrying and scurring through
there. We finally shut the thing down before I
really got a chance to use it very much. When we
powered it up there on the third day and we saw
that thing coming around there -and cage properly,
we compared the out-the-window attitudes and that
old attitude reference was right there. That's
when I got some confidence in the platform.
This is where we lost a couple of bets.
That's rignt. We lost a couple of beers on that
platform. At retrofire I had a lot of confidence
in the platform, but the first two and a half to
White
8.2 OAMS
McDivitt
White
McDivitt
three days I really didn't have anything with
which to establish any confidence. It was just
an unknown.
Jim did the majority of the work in this area and
I think his comments reflect my opinion also.
On the pad we did the thruster check that we
wanted to. We went around one whole cycle and
got nothing. We went around another whole cycle
and got nothing until we got to the last one.
We were going yaw left pitch-down, yaw right
pitch-up, yaw left pitch-down, yaw right pitch-
up. When we got to that second pitch-up, I heard
the thrusters fire for the first time.
You can hear them. It was very distinct,
That's right. And then we went around and yawed
left and they fired again. We waited 20 seconds
and fired a yaw left again, and they fired again,
These were the bottom manifold jets. We said,
"Okay, we're ready to go.", and that was the end
of it. So, it was a pretty straightforward check.
The inflight checks--I got my operational checks
on the OAMS systems while chasing the booster
around. I had Direct, Pulse, and Rate Command in
White
McDivitt
there as I chased it around, and those were the
only modes I intended to use right then. Later
on, I checked out the Reentry Rate Command and I
checked the Rate Command before we thrusted. It
did seem to be operating fine. Why don't you go
through the next part, Hi?
All right. We're going to get into the source
temperature and pressure, the regulated pressure,
and the propellant quantity. Let's take the
temperature first. The temperature of our OAMS
was 75 degrees all the way down the line. The
initial indications on the pressures were approxi-
mately 2800 psi for the source and 320 psi for the
regulated pressure.
The quantity gage operated all right except that,
as I mentioned earlier, the thing seemed to wander
up and down somewhere between 2 and 4 percent,
depending upon where you were in the mission.
You'd read it one time and it would be 60, and
you'd read it a little while later and it would
be 62, and you'd read it a little while later and
it'a be back about 60. ‘The greatest variation in
that thing that ever occurred was when I went to
sleep one time with it reading 60 and woke up and
White
MeDivitt
White
-@6 HEIDEN HAL T
we
it was reading 56. Another hour or two after that
it had climbed slowly back up to 60 again. I
had a long time to look at it in the same position.
When we ended the chasing-around at the end of the
first hour, we were down to 70 percent indicated
and we never got below 50 percent in four days.
I'll tell you, the position it seemed to stay
for days and days was 59 to 60 percent. We fired
in Pulse Mode for a long time with the gage at
that position, and all of a sudden that one time
it dropped down to about 55 percent,
But then it came back up to 60.
I guess it did, didn't it? The temperatures all
stayed fairly constant. If I recall right, they
dropped down to around 70 degrees. It seemed to
me they continually decreased throughout the
flight. I noticed this particularly in the RC5,
but I guess we'll get to that later. The propellart
quantity though, I think we mentioned earlier,
ended up on our gaging at about 43 percent at the
end. We got a little bit of ground information on
the OAMS propellant. I felt a little suspicious
of the gage when it kept staying there at 59 to 60
*
McDivitt
White
MeDivitt
White
MeDivitt
White
percent for so long.
We were pretty miserly with that OAMS fuel. We
set out to save the fuel and we sure did it.
I think that in future missions, if they permit
the crew to use the Pulse Mode in 4a saving-manner
they could do a lot more with the mission--if you
could use Pulse Mode instead of just free-drifting
around. In other words, line yourself up so you
can make some decent observations.
Shoot! We were in Horizon Scan Mode when we got
the last data, and I don't think we used any more
fuel than we were when we were in free drift.
That's right. We certainly got more out of the
orbit than we did when we were just drifting free.
I'll tell you one record that we ought to hold.
We've looked at the earth from more different
angles than anybody else in the world. Well,
maybe not. I guess the Russians did, but we sure
got a lot of different views of that earth as we
rotated around.
I think the ground information that they called up
on the status of our OAMS wasn't as much as they
could have called up to us, but I'm really satis-
fied that our OAMS was staying pretty constant.
SST eth 9
McDivitt So did I. The way I felt was that I knew that we
had to be as miserly with the fuel as we possibly
could, so we got as much out of as little fuel as
possible. There wasn't going to be anything to
change that velocity. We just went along and I
really didn't care how they were plotting that fuel
on the ground. I knew that we were starting to
get ahead of the schedule, because I was plotting
it roughly onboard the spacecraft. I could see we
were up above the line that we needed to remain
above to handle our OAMS retrofire.
White Actually, we followed the profile rather closely.
We leveled off there at first, and then when we
started using it, we went right down the profile.
MeDivitt We were a little below the line and we just held
the same fuel level until we walked out across it~
and got up on top of it Then, we went on down
above it.
White I think the controls and the switches were 211
satisfactory.
McDivitt I think so too. The attitude controller worked
fine and dandy. We didn't have any trouble with
it. The stick forces weren't too high. We didn't
get a chance to use it in any other mode besides
a
10
White
McDivitt
White
McDivitt
White
McDivitt
Pulse. It seemed to work all right in Pulse. I
don't really have any comments to make on the atti-
tude controller.
As a matter of fact, I didn't use any Rate Command.
Didn't you really?
We didn't use the Rate Command. I got to use
Direct a couple of times. I used Pulse a lot,
Everytime you'd go to sleep, I'd really have a ball
I could tell that by the wiggling.
No. That was really great--flying that spacecraft.
That's right, and I think Pulse is the mode. You
can do a lot with it. With a little bit of planning
you could get to the attitude--if you start out 5
or 6 minutes ahead of time. ‘That's what we were
doing. At 10 minutes before I was supposed to be
at a certain attitude I'd start, and one or two
little pulses and you'd--boop, boop, boop, boop--
the bad thing was if you were in an attitude where
you couldn't see the horizon and didn't know where
you were. You would give it a couple of pulses
and nothing would happen, and you'd have to give
it a couple of more pulses. It'd take a long time
sometimes before you would get to where you could
see. As a matter of fact, if at 5 minutes before
- =
White
WcDivitt
White
MeDivitt
11
we were supposed to be at a certain attitude we
weren't approaching it, I'd start pulsing a little
harder.
You'd hear a series of about five quick pulses.
It was a very economical control mode,
The maneuver controller worked the way it was
supposed to.
What about the deadband? Did you think the dead-
bands and breakouts were all satisfactory?
Yes, just like the one we used in the simulator.
You've got a lot of slop in it when you're making
gross maneuvers because you're not fixing your
elbow and manipulating around that point. You're
fixing your shoulder and your whole arm, and
it's just like shoveling coal--you've got about
that much finesse to it. I don't think there's
much you can say about it. The controls weren't
too gross and they weren't too minor. The whole
thing was adequate. We did have an inflight mal-
function, or irregularity. We were in Horizon
Seanner Mode one time and Hd wanted to yaw around.
He started to yaw and the thing rolled. The
Horizon Scanner Mode fired the roll thrusters to
level it back off--
12
White
McDivitt
White
McDivitt
McDivitt
I couldn't get the yaw. We had a circuit breaker
off.
Finally, after you did that a couple of times I
looked up and saw we had knocked a circuit breaker
off. That was one thing that we didn't cover in
EVA that I should have mentioned. Ed was a real
hazard to the switch positions in that he was all
over with his feet, arms, and hands --.
I don't think I threw any though. Did I? Come
on now. Youtre not guilty wntil you're convicted,
I don't know. You kept putting your foot on the
HF Reentry Antenna Switch and stepping on it.
Ha. Ha. Ha,
As for the attitude control modes--I mentioned
the Rate Command in OAMS seemed to be tighter than
the Rate Command in RCS, although they use the
game electronics, the same gyros, and the whole
thing. It might have just been my imagination,
put I felt that the Rate Command system in RCS was
a lot looser than it was in OAMS. The Reentry
Rate Command operated just the way it should. It
had a 4 degree deadband, and handled the spacecraft
very well during reentry. Direct had a lot more
authority than I thought it would, but it was
13
pretty straightforward. I think Pulse was the
best mode on the spacecraft for the orbit phase.
We were able to save all kinds of fuel, it worked
fine, and it was just about what the doctor ordered,
We didn't use the Horizon Scan Mode during about
the first three days of flight, except for the second
orbit when I think I was in Horizon Scan so that I
could have the freedom to help Ed prepare for his
EVA, The last day we used the Horizon Scan Mode,
and I found it to be an excellent mode. There was
only one case when it broke lock and didn't recover,
Wasn't that it, Ed?
White You've got it in the book.
MeDivitt We've got in the book and we'll check on that.
The Horizon Scan Mode worked essentially for 24
hours without any problem .and I think it's an
excellent control mode. It seemed to be very
economical on fuel. We were doing a lot of
yawing around and right at sunrise and sunset it
seemed to get a little nervous, especially if we
had the horizon scanner pointed within about plus
or minus 45 degrees of the sun. The moon didn't
seem to affect it at all. I noticed that, occa-
sionally, we would get some thruster blips with the sun
weetsHDEN Ata
White
McDivitt
White
McDivitt
White
McDivitt
pointed toward the horizon seayiien although we
never got an unlock light, We wouldn't get an
unlock light, but we'd get a bunch of maybe four
or five thruster blips right there.
Particularly at sunrise.
It would hold. I thought the Horizon Scan--
It was definitely getting some spurious signals
through but not enough to break it out all the way.
I thought the Horizon Scan Mode was an excellent
attitude-hold mode.
Did you notice the water boiler venting, Jim?
Yes, I did. We kept yawing around to the left,
I believe it was left. I did notice the fact
that we were yawing, but not very much. We were
yawing at rates that were extremely low and it just
took a pulse every once in a while to handle the
thing. As a matter of fact, when we were chasing —
the booster around a lot at the beginning, I never
even noticed. It was when we were in the Pulse Con-
trol Mode for a period of time, when we didn't do much
thrusting in yaw,that I noticed we did start drifting
off in yaw. ‘So I did notice the water boiler venting.
White
McDivitt
ee Tee
= -
I didn't think you noticed it earlier when we
were working.
Well, I did notice it a little bit in that first
orbit, but it wasn't distracting at all. It would
just drift off a little bit and I'd whop it and
it would be back. At SECO + 40, I used the trans-
lation thrusters to damp the booster-spacecraft
rates. One of them was a little higher than the
other, although they were both down in the order
of a half of a degree/second. I did fire one
thruster one time or possibly two times to damp
the rate. I don't know if it was pitch or yaw.
You know, you are working in spacecraft pitch and
booster yaw and spacecraft yaw and booster pitch.
I was getting my coordinate system transformed
around in my mind, going from booster coordinate
system to the spacecraft. I don't remember
whether it was yaw or pitch, but I did thrust
once or twice. By the way, I could hear those
thrusters fire. At SECO + 30 I said, "Thrusting,"
and I started thrusting. "Separate", and Ed
punched the SPACECRAFT SEPARATE. We were in Direct
and I thrusted straight ahead for about 5 seconds.
Then I went back into Rate Command. Separation was
16
White
McDivitt
just smooth--we didn't come off with a rotational
rate.
I think one of the things you might comment on, Jim,
is that you fired most of those thrusters during
that initial time.
I'm sure I fired the upward-firing thrusters a
number of times. That isn't any more difficult
to control than the other one. Actually you can
fire these thrusters whether you are in Rate
Command, Direct or even in Pulse. When you fire
them, you get a rate and you just damp the rate
out with the attitude controller. When you are
firing the translation thrusters, the things that
you really hear are not the translation thrusters,
but the attitude thrusters. Those translation
thrusters are really tough to hear, but the atti-
tude thrusters are very easy to hear. I don't
understand why. They must be mounted differently
because their location isn't that much different.
I think I fired the aft-firing thrusters a couple
of times and they didn't make any more noise than
the forward-firing thrusters, that I could tell.
The up and down and left and right ones were just
as easy to fire as the other ones. Our OAMS retro
was 127 feet/second which, incidently, happened
to come out exactly 2 minutes and 40 seconds. I
suspect that we selected OAMS retrofire on the basis
of time, rather than on the basis of AV.
White Very convenient, wasn't it?
McDivitt Very convenient. It was obvious there is no more
difficulty in timing 2 minutes 40 seconds during
our OAMS retrofire than it is during any other
thing. We had no trouble with it. I was convinced
that when we got through with it, that was really
the proper conversion factor between AV and AT.
We had exactly 127 feet/second, and we sure had
the time nailed down.
8.3 RCS
McDivitt The operational checks that we did on the RCS
occurred at about TR minus an hour. When I checked
the system out it seemed like I had a lot less
authority and a lot sloppier Rate Command than TI
had in OAMS. The operational check consisted of
pitching up and down, yawing left and right,
rolling lef+ and right on each ring in Rate Command
and Direct. Direct worked as I expected it to.
In Rate Command, however, as I pitched up and down
I noticed that my top left yaw thruster was doing
White
BOnFPERT AS
a lot of firing, too. I started out checking the
Rate Command, so I thought I might possibly have
one bad pitch thruster that was causing a rolling
moment that was being counteracted by the yaw-roll
jets. When I did it in Direct, however, it wasn't
doing that. It wasn't rolling either, so I felt
that it must just be a very tight deadband that
was trying to hold us in there. So, the operational
checks were all right. The only thing we had to
monitor on the system was the temperature and the
pressure of the propellant, t seemed to hold
pretty well.
I have some comments on that. I kept a running
log of them as we went along. The temperature
started out at 75 degrees and 3000 pounds. It held
that way pretty well until about the 65th hour, when
the temperature gradually went down. The temperature
decreased to a point where we started getting the
RCS heater lights that we noted earlier. We got
about eight series of RCS heater lights. It took
about 5 minutes to extinguish the light. It was
the A-ring,then the B-ring, and then the A-ring.
It seemed to alternate each time back and forth and
it came on for about 15 to 20 minute periods of
-GONFIDENTHE
McDivitt
White
19
time. It started right after a night cycle, It
seemed rather natural to me that there wasn't
really something wrong, but that we actually had
a cold RCS thing out there and it did need some
heat. After heat was applied it did appear to go
away. I decided to go ahead and set up a slow roll
rate in the daytime, and I kept that roll rate in
for several orbits. Whether this actually helped
to get the light off or not, I don't know. We
didn't get anymore lights after this time. I think
there ought to be one other comment on the RCS,
and that is the temperatures and the pressures
stayed up pretty well except when we actuated the
system. The pressures then went down further than
we had expected them to go. They went dow to
2400 to 2500 psi. This was a little lower than I
expected to see,
I think the pressures in the RCS A and B dropped
by about 100 pounds throughout the four-day period.
They were slightly over 3000 pounds and they got
down to slightly under 3000.
The lowest temperatures I noted were in the neigh-
borhood of about 63 to 64 degrees. They started
out at 75 degrees.
20
MecDivitt
White
McDivitt
White
MeDivitt
White
McDivitt
ea inna
Let me ask you a question?
Yes.
When you turned on the RCS heaters, did you turn
on the heaters on both rings, or did you turn on
the RCS Heater Switch and then turn off the circuit
breaker on the other ring?
I turned the heaters on and then I checked to see
which ring it was that was actually heating up by
using the circuit breakers. The first time I went
ahead and left them on and then the other ring
came on. I felt that one of them was about as
cold as the other, so I left the heaters on both
rings throughout the heating cycles.
Good.
They were in perfect sequence--A and B, A and B,
and about 15 minutes apart. The regularity was
surprising. The temperatures at the time when
these lights came on were indicating about 63 or
64 degrees and it seemed like it would come up a
little bit, and then come right back down and pop
back on again. I felt it was not an actual
temperature problen.
I used Rate Command, Reentry Rate Command and Pulse
control modes, I didn't use Direct. They all
COMABEN Td
White
21
operated as I thought they should. I've already
mentioned I thought Rate Command was a little
sloppier in RCS than it was in OAMS. It certainly
did a fine job of holding the retro attitude during
retrofire. Retrofire attitude control was excellent.
We didn't deviate more than about a degree from
the attitude we were supposed to hold, and I had
plenty of authority there. From my standpoint
it couldn't have been any better. I was really
happy about it. I used the Reentry Rate Command
with roll rate gyro off, so that I had essentially
Direct in roll and Reentry Rate Command in pitch
and yaw axes. It had the typical 4 degree deadband
that it was supposed to have. It did do rate damping
as it was supposed to, It performed just the way
it should. Ed, you want to cover that heater-lights
thing again? I think you've already got that thing
pretty much in detail.
I have the precise times at which the lights came
on. It started at about the 64th or 65th elapsed
time hour. At 06:47, the first light, in the A-ring,
came on. At 06:25 the A-ring light came on again.
That was the last time. During that period of time
the A and the B-rings cycled on and off inter-
22
8.4
McDivitt
SADE HAtey
mittently.
During descent, we turned the power off to see if
the drogue chute was unstable. It wasn't. We
turned the power back on and the propellant valves
off and burned up all of the fuel in the manifolds,
We had no fumes after impact.
Environmental Controi System
MeDivitt
White
MeDivitt
White
McDivitt
I thought the suit mobility was as good in the
spacecraft as it is anywhere else. I think these
suits are pretty good suits. I didn't find any
trouble with them whatsoever in the spacecraft
that I wasn't already aware of. The pressure held
up good. I did a pressure check on the suit. It
bled down about 0.2 or 0.4 psi in about 30 seconds,
which really wasn't too bad. The temperature was
always good. It ran between about 50 and 55
degrees diring the entire flight except when we
really worked hard. I don't think it ever got up
over 60. Do you, Hd?
No,
We had reasonably good temperature control.
The cabin temperature got up pretty high one time
and then it came back down.
Yes, on about the first orbit.
Sen h bE Hae
White
MeDivitt
White
MeDivitt
23
That's r ght. It got up to about 90.
100, it was. We turmed the cabin heat exchanger
on for just a short time and it went right back on
down to 80 degrees.
It stayed in the area of 82 to 83 degrees the whole
flight.
The humidity in the suit must have been pretty dry
because my foot dried out. I didn't take any wet-
bulb readings inside the suit. The CO, stayed at
zero all the time. It never did go up except when
we'd go to 0, High Rate, when it would bound off
the top peg and fall back down again. The comfort
and suit controls were pretty reasonable. ‘The 0,
demand regulator seemed to work all right. My
umbilicals were short. My fingertip lights were
lousy. Before launch I only had one that worked. ,
On my right-hand glove one of the bulbs obviously
didn't work. One of them did work. On my left-~-
hand glove the switch on the batteries would only
turn the lights on if it was in one exact position,
woich wasn't full throw in either direction. So I
found out I had only one fingertip light that
worked. However, during the flight I didn't use
my fingertip lights except one time when I used ~
SOnrFDENTIAT—
24
them for a flashlight. I had my gloves off and I
reached over and got my gloves and turned the
fingertip lights on and shined the gloves on some-
thing. I didn't use them a lot. I do want te
comment on one thing, though, since we're talking
about the suits here. JI launched without the plug
that goes in the blood pressure port in the suit.
I don't feel we should launch these things with
no plug to plug up the blood pressure port in the
suit, especially when we're going EVA. I think
that was a mistake. The only pressure points I had
in the suit were in the helmet. Those were just
above my ears where I tended to move my head back
and forth within the helmet. I finally rubbed up
all the hair so that it was going in the wrong
direction. When you press against hair for a long
time in the wrong direction it becomes very uncom-
fortable. At about the end of 2 3/4 days I took
my helmet off for a couple of hours, and it felt a
lot better. The only problem is that when you have
your helmet off there is no place to stow it. We
had the foot wells full of gear, so when I had the
helmet off I just let it float around on my lap,
and over in Ed's lap. There wasn't any place to
CONFIDES -
White
25
put it. The micro-meteroid blanket that I had
strapped under my right leg wasn't a detriment.
As a matter of fact since we had no place to stow
it, I just left it strapped to my leg wntil reentry.
Then, I felt that if we had to get out in the water
I didn't want to have any straps hanging off me
that I didn't need. So, I took it off and threw
it on the floor along with Ed's sleeves. I don't
have anymore comments on my suit.
I wore the EVA suit. I think the mobility of the
suit was about what I had expected. Actually, I
think the mobility in some respects was a little
better, and in some respects it was a little less
than I had expected. I wasn't able to get into the
right-hand aft food box as well as I had thought
I was going to be able to in zero g. In fact, the —
position that I had figured out to use, which was
leaning forward and reaching in backwards with my
left arm, didn't work out well at all. I had to
actually turn around 90 degrees in the seat and
reach in with my right arm, This worked out all
right. I was able to get hold of things in the
box. The surprise that I got though, was that I
could get into the right-hand aft refuse box much
26
McDivitt
White
White
MeDivitt
White
McDivitt
White
FOMABDEN FAL
easier than I had thought I'd ever be able to. It
turned out that I was able to get into that box
easier while in orbit, by far, than--
It's a rubber covered box.
It's a rubber covered box on the right hand side.
I think that box does have the capability of stow-
ing refuse in it and stowing some things prior to
launch in it, too.
Did you try that box during flight, Jim?
Yes, I did. I didn't find it easy to get into.
I thought the things we had stowed in it were
real good things--items that we didn't need at all
in flight and possibly might not need--
I used all four defecation bags that I had on my
side. I used them up during flight. In fact, you
used one of them.
That's right, we did have a bag of those defeca-
tion bags out. It just happened to be over on my
side where you could get to it.
You were asleep. I had to get them or wake you up.
I pressure-checked my suit. I checked it at 8.5
and it bled down several tenths of a psi. I was
satisfied with the pressure-holding of my suit.
eT
There was one thing though with the suit that I
wasn't too happy with. I was hot all the time
in the suit. It got so that after a while I got
used to the normal temperature as being warm.
I could increase the temperature, which seemed
rather strange to both Jim and me, by putting out
my gloves and closing my faceplate. I could go
to sleep. At that time my temperature would go
up considerably inside the suit. It seemed like
I could stay in there only an hour or an hour and
15 minutes and rest before I had to either open
up the faceplate or do something else. So, the
temperature got uncomfortably warm in about an
hour or an hour and fifteen minutes with the face-
plate closed, the sleeves on and the gloves on.
The humidity in the suit, I thought, was quite
dry. I had quite a tendency for my lips to crack
and my nose to get very dry. In fact, I noticed
my nose was itching considerably. This was an
indicator to me every time I would go to sleep.
I would wake up with my nose itching and feeling
quite hot and uncomfortable. My lips got to the
point where I thought they were going to crack,
28
— arene :
and I was trying to be very careful and keep them
from cracking and getting anymore uncomfortable
than they were. Jim mentioned the CO, sensors
stayed on zero, which I was happy to see. I
think one thing that I was fairly happy about was
that the suit, as bulky as it was, wasn't depres-—
singly uncomfortable. I felt that I did have a
pretty heavy suit on most of the time, and I was
a little bit constrained in my mobility. The
idea to have the detachable sleeves that I could
take off after the EVA work was, I felt, a very
good decision. I felt much more comfortable,
and I had a much higher degree of mobility around
with my arms in the spacecraft. It was not as
tiring to move around as it had been when I was
inside the heavy sleeves. So, I was quite happy
to take them off. We took them off, I believe,
shortly after my first sleep. I slept with them
on the first time, and then we took them off. I
think they were quite easy to take off. As a
matter of fact, I think if you went EVA at a
later time you could take those sleeves onboard,
and if they were made just a little easier to
Slip on and off over the wrist, you could take
CORED ESTIAT
McD; vitt
White
them on and off in flight if you wanted to,
I don't know. I'd hesitate to recommend putting
them on in flight. It might get pretty tricky.
I think if you put them on in flight, you'd want
to put them over all the harness, rather than
under the harness.
That's exactly what I was going to say. I think
if you took the life preservers off, you could
actually make the sleeves big enough so that you
could slip them on and velcro them across the
back over the harness. This might be for the
type of operation of throwing equipment in and
out. I think in the future, though, a suit as
heavy as this might not be required. The controls
and the switches in the suit, I felt, were satis-
factory. There wasn't anything that I couldn't
get at in the spacecraft. It was easier under
weightless conditions for me to operate certain
controls. In fact, I think I was able to get
down and unscrew the bellows in the gun hose as
well and maybe a little easier than you could,
Jim. At least initially, I was able to get down
there. Of course you weren't really particularly
trying to do it at that time.
30
McDivitt
White
McDivitt
White
I suspect I probably could have gotten down there
as easy or easier than you if I had really gotten
around to trying.
I don't remember, but, anyhow, I was surprised
with the ease which I had in getting down.
We were trying to dump the pressure in the bellow
before we went EVA with it.
Right. The demand regulator was satisfactory. My
umbilical ;I thought, was very easy to use and
disconnect. I was quite happy to have the micro-
dot in there. One comment on the micro-dot--the
first time we exercised the micro-dots on our
suit, they were pretty hard to operate. Mine got
progressively easier to use each time I used it.
The fingertip lights that I had were better than
Jim's. TI had lights with Lexan tops on them.
All my lights worked, and {[ felt that their
operation was quite satisfactory. We had decided
to put my lights between the first and second
joints for several reasons. We thought the EVA
gloves would be easier to don and there'd be less
tendency to break them. I think, though, the
position of the lights was still a little too far
forward if it was intended to put them back between
BORE Tat
“SSE q
the first and second joints, because the lights
were resting right on top of my first joint. I
think if I had worm BY gloves anymore, I would
have gotten a very sore first knuckle. If you
are going to move them back, I think they should
definitely be moved back behind the first knuckle.
MeDivitt Where were they getting you, Hd?
White ' Right on the top of the knuckle.
McDivitt You think they ought to be back?
White If they are going to be anywhere, they ought to be
back here, and I'm not too sure that is necessary.
In fact, I think the best place is behind is
fingertip and in front of the first joint.
McDivitt But, with the plastic covers over the gloves,
White With the plastic cover on the glove, and I think
we've got the right position for the lights. I
don't think they should be back behind the first
knuckle. I think they should be in front of that
first knuckle and behind the fingertip. That's a
good place for them. That's where we've been using
them in the past. I think the Lexan cover
on the light bulb is a darn good idea.
McDivitt Yes, I think so, too. Shoot! I checked my lights
before launch and found out that I already had one
SMD EN TIT
32
White
of them out on my right hand. I wasn't too happy
about it.
I was a little disappointed. I think the only
discrepancy I found in my suit was that I had no
blood pressure plug either. A point that I was
pretty happy with was that I had no pressure points
from my suit at all on my body, T had one set of
pressure points from my helmet pressing down on the
front forward part of my head. I knew why this
was. I'd had Joe Schmitt adjust my cables so that
I could pull my helmet down to a maximum amount
for the EVA work. I felt that I just bought this
discomfort by having my cables adjusted in this
manner. It was pretty uncomfortable though. I
checked out the use of the emergency bottles on
the EVA equipment and they worked as they were
supposed to. I was able to regulate the flow.
Incidently, before I went out the reading on the
EVA bottles was full-scale, 3400 pounds. I was
happy to see that. All in all, I was quite happy
with the suit. I think it was a very well designed
suit and it met the requirements that were levied
upon it. It was a heavy suit and a big suit to
wear for four days, but I felt the suit wasn't as
35
bad as I had expected it was going to be.
I have one more comment. I'd like to comment on
the inner liner. We decided to go with the inner
liner. in and I felt this was a good decision.
The inside of the suit was comfortable, and I
didn't get any pressure points. I think one reason
why neither Jim nor I got any particular pressure
points from the suit was that we had worn these
suits a heck of a lot of time. I had over 50
hours on my flight suit. I don't know how many
hours Jim had on his.
34
McDivitt
White
Actually Hd had just finished talking about his
inner liner. I'd like to comment about the inner
liner too. I thought about it when he was talking
about his. I think that was one of the really
wise decisions *- to go with that inmer liner.
I felt that it offered a lot more comfort than
wearing that rubber suit up against my body, or
up against my underwear. I sort of felt that I
was really quite comfortable in this suit. I
didn't find my mobility limited by my inner liner
at all, and I had made sure that it fit. I think
that has a lot to do with it.
I worked the suit once for about a four~hour
period with just the rubber inside. I did no-
tice it sticking to me, and I didn't feel as com-
fortable. After I got inside the suit with pres-
sure on my body, the suit felt pretty darn good.
I had the knees cut out of my suits. The knees
are still teo short. Having been in it for four
days, I know the dimensions are wrong. The di-
mension from my knee down to my foot is not long
enough. Jt's not just the inner liner, but the
+a
McDivitt
White
McDivitt
White
McDivit-
White
MeDivitt
White
35
link net in itself just isn't long enough.
You wouldn't say you had a pressure point though?
No, it was just a constant pull on there all the
time.
Did it bother you very much during the flight?
Yes, it bothered me a little bit.
So you really did have sort of a pressure point
then?
Yes, to some extent in that area. I had had that
one so much before. It had been so extreme in
some cases that it really didn't bother me too
much.
Both of us should mention something about the
visors.
I thought you ought to mention something about
your visor problem, your EVA visor or the Hie
one.
Well, I have briefed the visor on the EVA pretty
well. The one that I will mention now is the
visor that I had on my regular helmet. I thought
that the vision through it was quite good. I
noticed no distortion at all through it, but I
did immediately put a couple big scratches on it
CON AB ENS rete
36
MeDivitt
Gh EE He
in the beginning when I was unstowing equipment.
I continued to scratch it throughout the mission.
When I finished, the visor was considerably
scratched up as you would probably notice if
you looked at my suit. I don't know what there is
to do about this other than to accept a scratchy
visor.
If you've got the visors down in front of your
face, you don't tend to scratch it up as much.
I think it was really worn out because you
started opening up your visor and leaving it up
over your head a lot earlier than I did. At about
the two and a half or three day mark, I looked at
your visor and it was really a mess. I took the
helmet off and cleaned the visor because it was
dirty on the inside and the outside. I looked at
my visor and had very few marks on it. I had a
few little scratches, but very minor. Then I
started putting my visor up more and more be-
cause they wanted us to stay open. Because I'm
a lot taller than you are, I really started beat-—
ing mine up. In the last day, I think I caught
up with you and maybe even surpassed you in the
White
McDivitt
White
McDivitt
37
amount of marks on it. I'll say another thing.
I'm sure glad we didn't go in for those Lexan
visors that they wanted us to fly with, cause the
distortion would have driven me batty in about
the first six hours.
I think you must insist on perfectly optically
clear visors.
That's right. You've got to have good optics.
I took my helmet off about three times, and I
didn't leave it off very long.
I took mine off about two times. I took it off
one time for an hour because my hair right above
my ears was really bothering me. I didn't bother
getting a light-weight headset out, and when any-
bedy called me, I had the thing sitting in ny
lap and I could hear it. I took one of the ...
and pulled it back and I hollered into the mike,
Ha, ha!, till I could hear it. I said, "TI tye Zot
my helmet off. Unless you've got something im-
portant to tell me, don't bother me." Ha, ha!
And he said, "Okay." It was one of those passes,
you know, where you only talk to one guy for about
an hour. Then I took it off one other time for
about a half hour to rub my ears. I was quite
fot vb | TS Td) A ;
38
White
McDivitt
comfortable with my helmet on for two days.
Do you want to know something that's kind of
strange? I was more comfortable with my helmet
on than off. In fact, I kind of got used to
those pressure points on the top of my head with
the helmet on. When I took the helmet off and
moved my head around, I felt a little dizzy from
not having these restraints. I didn't feel as
comfortable as I did with my helmet on. The times
I had my helmet off were when I was running D-9.
I ran the D-9 Experiment several times with my
helmet off so I'd have better use of my sextant.
I took it off one other time near the end when
they indicated they would like to have every-
thing off. I didn't feel particularly comforta-
ble with my helmet off any more. I got so used }
to having that thing on that I put it on so I
could talk better with the stations. They were
calling me from time to time, and I thought it
would be a little better. Before I forget, I
think the portable headset is really a lousy
design.
I coneur. I think it ought to be thrown out.
White
McDivitt
Sern 5:
39
T've seen the ones they've got in the MCC and
they're good plain old headsets. I don't see
any reason why we can't get one that stays on
your head and stays in your ear. You put this
thing on and it pops off about two minutes later.
It's not built to stay on my size head and I
noticed it didn't stay on Jim's very well either.
I think the portable headset idea is 4 good
idea, but we ought to have a good headset for
it. Okay. As we mentioned earlier the cabin
pressure relieved at about 5.5 and held that
way during launch. It went back down to 4.9
or 4.8 and this is where it stayed for the re-
mainder of the mission. I think that they prob-~
ably overshot their zeal to correct the cabin
pressure that John and Gus had had on GT-3 and
put ours down so that it was actually relieving
lower and sealing lower than it would have been
desirable. I was expecting it to seal up around
5.5 or 5.7 like it was advertised.
I checked my suit gage against the cabin pres-
sure gage and my suit gage read higher than
the cabin pressure gage by about .3 of a pound.
= i
40
White
McDivitt
White
McDivitt
White
McDivitt
White
Yes, mine was right on it though.
I know. You checked your suit gage against
the cabin pressure and yours read just about on
it, didn't it? Was it a tenth of a pound higher
or was it right on it?
Right on.
Okay. So mine was reading a little higher,
indicating to me that possibly the cabin pres=
sure was higher. But since id's read with it,
I don't know where we were.
Well, the pressure at which it relieved at went
right into the problem of the temperature-pres-
sure relief in the cryogenic oxygen system so
that those two problems kind of lashed together,
The venting in the 0, system was set at around
2
970.
967, I think the poop sheet said.
Well, it was about 967 or 970. We had the pos-
sibility of losing oxygen in a steady manner
out of the spacecraft if we let the pressure
rise up above--well, the ground felt 960, and
I concurred with that figure. So throughout
the flight we had to keep venting our 9, system
MeDivitt
White
41
down so the pressure would remain down below
960. They initially told us to vent it to keep
it at 930 to 960. Then they told us to vent it
on down to about 890. From then on, we vented
it down in the neighborhood of between 890 and
93, depending upon who was asleep and who wasn't
asleep. It sure seemed to be an unsatisfactory
solution to two problems--one of the cabin hold-
ing at a higher pressure than they wanted it to
on GI-3 and also the problem of the 0, system
venting outside of the pressure gage. In the
oxygen system I think the solution to putting
the venting down at 967 was a poor solution to
the problem of having a poorly designed gage.
I think the gage was again poorly designed and
it should be designed to read about 1200 sana.
Relief should be up in that area.
If they really went ahead and jacked down the
relief pressure, to get it on the gage, I think
that is one heck of an approach to an engineer-
ing problen.
I think that's a gross thing to do and if they
did that deliberately, I think they deserve a
42
MeDivitt
White
MecDivitt
White
McDivitt
White
McDivitt
very black star for that one.
They need their heads examined!
I guess we beat that one around pretty well,
didn't we?
Yes. The way that we were venting the cabin
was by going to 0; High Rate and venting the
oxygen out through the cabin vent or going to
cabin repress and using up the oxygen through
the cabin and through the cabin vent valve
that way.
T was quite satisfied with the cabin temperature.
It started out and got pretty hot at one time
early in the flight and went up to 100 as you °
noted,and then it went back down into the 80's.
I think it actually dropped into the 70's a ¢ime
or two.
That's right. It was in the 70's most of the
time,
Right.
Let's get the data book, The dry bulb tempera-
ture was 80; 80, the first time we tood it.
Then it was 79, 79, 79. Then it was 75, 75,
75, and then they stayed between 75 and 77,1
White
McDivitt
White
McDivitt
White
McDivitt
45
think, the rest of the flight. No, here it is
down as low as 72. So it got down to around
72 late in the flight, and here we are with a
whole bunch of 70's to 73's and a couple of 76's.
So I guess that 75 was the average temperature
throughout the whole flight.
I think our cabin temperature gage was reflect-
ing a little higher temperature than these.
No, let's see. It was down around 75.
It went down to 74 at one time, I remember.
Yes, I think 75 was a good average cabin temp-
erature for the whole flight.
I thought this was a pretty satisfactory cabin
temperature. The suit temperatures were also
down. They stayed down from about 52 to 54
most of the flight. I thought that was a pretty
satisfactory temperature there. I believe that
there was a difference in suit temperatures be-
tween Jim and me because I was continually
hollering about being hot. I think that temp-
erature-wise Jim was relatively comfortable.
I was very comfortable, and as a matter of fact,
when I went to sleep, I tended to get just a
44
White
McDivitt
White
little bit cool, especially if I had urinated
all over myself.
I don't remember one time during the flight
during which I was cool in the suit. I think
I was hot most of the time in the suit. I got
used to it after a while. The only time that
it was not satisfactory, as far as I was con-
cerned, waS when I was trying to sleep. The
humidity data that we got doesn't go along with
what everybody was expecting.
No, not by a long shot.
No, not at all. Our little gage seemed like
it was working properly. We didn't have any
visible moisture at any time at any place in
the spacecraft. It seemed to be indicating
down around 62 to 63 percent relative Hanteey
which was a big surprise to myself. With this
type of data, I began going open faceplate and
open gloves fairly early in the flight, about
a day or a day and a half, and continued in this
manner just about throughout the flight. We
used the wrist dams quite a bit of the time.
But I had my faceplate open with my wrist dams '
Context
This is one of 40 NASA records in the declassified archive, reported in the Other region. It was published in Release 03 (6/12).
Evidence tiers describe the type of record (sensor capture vs. written report vs.
administrative file) · not a claim about its conclusions. UFO Papers reports only what the documents state.