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Gemini 4 Experiment Debriefing, 1967

National Aeronautics and Space Administration · 1965 · 224 pages · text from the file's own layer

This NASA file from 1965 combines Mission Operation Report M-913-65-04 on the Gemini 4 (GT-4) flight with related correspondence. Memoranda from the Associate Administrator for Manned Space Flight describe the planned four-day mission with James McDivitt and Edward White, including a spacewalk, a rendezvous with the booster second stage and thirteen experiments. Later letters and telegrams from NASA's Manned Space Science office concern the astronaut debriefing and requests for GT-4 photography and film for scientific analysis.

From the source:Release of 2026-06-12 Incident: June 3-7, 1965, Low Earth Orbit. Gemini IV was the second crewed mission of the Gemini series. Astronauts James McDivitt and Edward White successfully completed the four-day flight between June 3 and June 7, 1965. The mission included the first American spacewalk. This collection of documents contains a transcription of the astronauts recounting their observations of bright particles outside the spacecraft, dated circa June 25, 1967, on pages 78-81, and page 101.

••
-
M-913-65-04
aviator assignments including a three year tour as a test pilot at the Naval Air
Test Center at Patuxent River, Maryland. His duties there included service as
program manager for the F4H Weapon System Evaluation. Lovell was graduated
from the Aviation Safety School of the University of Southern California. He
served as flight instructor and safety officer with Fighter Squadron 101 at the
Naval Air Station at Oceana, Virginia. Lovell has logged 3,000 hours flying
time, including more than 2,000 hours in jet aircraft.
Love II was selected as an astronaut by NASA in September 1962. In addition to
participating in the overal I astronaut training program, he has been assigned
special duties. These duties included monitoring design and development of
recovery and crew life support systems. These include space suits, environmental
control system and developing techniques for lunar and earth landings and recovery.
The launch trajectory
for the GT-4 mission
wi 11 be similar to that
flown by GT-3. ln-
serti on wi 11 be at the same
altitude, 87 miles, but
the first apogee of GT-4
will be 161 miles. The
Gemini launch sequence
is shown in Figure 20.
FLIGHT PLAN
In addition to the various
orbi ta I maneuvers to be
pe rformed during the mis
sion, as ca Iled out in
Table II, other activities
will be taking place as
is shown below in Table
111, a summarization of
the Flight Plan. The
consumable items loaded
onboard the spacecraft
are shown in Table IV.
TRAJECTORY
811Ul
MODE 111: SHUTDOWN
j •SEPARATE SIC
5:10 CHANGE -·-·- •RETRO &REBffllY
A200.m ABORT MOOl SEflllNCE
L 2:48 START 11:SHUTDOWN
T RADIO GUIDANCE j.SALVO RETROS
.
1:40 CHANG
ABORT MOOE
1:19 MAX Q
2:34 BECO ~.ET11SON RETROI 5.5G·s •=SEOllll:ET
U 75,000' 1·-
~ 42.000' IIElAYEO AQIE U:SfUTOOWN
•WAIT 5 SECONDS
25.000' •SALVO RETim
•JETTISON RmO
SECTIII0:50 CHANGE ABORT····-···-·15.000' •I.AIIN SBIIIIGMODE
Q:23 START PITCH2500'
Q:20 STOP ROLL 012• l:EJECT2000·
~l Q:10 START ROLL oas·
:OO LIFT OFF-- ... - _______...
0 50 •
RANG -NAUTICAL MIES -FIG. 20
• 5/24/65 Page 13

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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 224 pages are in the text index: search them above, or from the library's search.