PROJECT GEMINI
COLLECTION
PROJECT GEMINICOLLECTION

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Gemini Spacecraft

The machine behind the mission

Gemini Spacecraft

  • 1965–1966
  • 10 crewed flights
  • Launched from Cape Kennedy

Two seats, an onboard computer and a docking target. Gemini is where America learned to rendezvous, spacewalk and stay up for two weeks — the dress rehearsal for the Moon.

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THE BRIDGE TO THE MOON

Ten crewed flights in twenty months taught Apollo everything it couldn't fly without: rendezvous, docking, spacewalking, endurance. Spaceflight stopped being a stunt and became a discipline.

THE UNSUNG REHEARSAL

No lunar landings, no famous quotes — just relentless skill-building where America pulled ahead. Our Gemini collection respects the rehearsal behind the glamorous leap.

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SHOWING 2 OUT OF 2 PRODUCTS
SEDR 300 - Gemini Familiarization Manual

Gemini, by the numbers

Figure 1-1SEDR 300
Spacecraft - pre-launch configuration
19 FT7,100 - 8,300 LB

Two men side by side in a cabin the size of a sports car front seat.

Spacecraft - pre-launch configuration

Figure 16-1SEDR 300
Typical use of EVA equipment
23 MINGT-4 - 3 JUN 1965

Ed White on a 25-foot golden umbilical. He did not want to come back in.

Typical use of EVA equipment

Figure 13-1SEDR 300
Docking system
16 MAR 1966GT-8 - FIRST DOCKING

The nose slid into the Agena cone and three latches caught: the first docking in space. Within the hour a stuck thruster had them tumbling.

Docking system

DID YOU KNOW?
PROJECT GEMINI

FLIGHT PLAN

GT-3 THROUGH GT-12 - REF. SEDR 300
FINAL

Ten crewed flights in twenty months. Rendezvous, docking, spacewalking, two weeks in a front seat. Drawings in this book are from the McDonnell familiarization manual the crews trained on. This book is the record.

PREPARED BY
FLIGHT PLANNING BRANCH
CAPE KENNEDY CLOTHING
PORT ST. JOHN, FLORIDA
Artie RedstoneChief, Flight Planning Branch
Max QChief, Flight Crew Support Division
Turn the page →
MCC-H

Figure 1-1SPACECRAFT PRE-LAUNCH CONFIGURATION

NOTES
SPACECRAFT PRE-LAUNCH CONFIGURATION
Tap the drawing to enlarge

Nineteen feet long, 7,000 to 8,300 pounds depending on the flight, two men side by side. Gemini was built in sections that came apart on purpose: the adapter stayed in orbit, the retro section burned off, and only the re-entry module came home under the parachute.

  1. 1Rendezvous and Recovery section - the rendezvous radar, the drogue, pilot and main parachutes. Jettisoned after re-entry.
  2. 2Re-entry Control System section - the small thrusters that steered the capsule through re-entry.
  3. 3Crew and equipment section - the pressurized cabin. Command pilot on the left, pilot on the right.
  4. 4Retrograde section - four solid rockets fired in sequence to bring the spacecraft out of orbit.
  5. 5Equipment section - fuel cells, maneuvering propellant and the cooling radiators. Left in orbit at retrofire.
  6. 6Titan II launch vehicle - about 90 feet without the spacecraft, 109 on the pad, 10 feet across, 430,000 pounds of thrust on hypergolic propellants that light on contact.
Spacecraft
Length19 ft
Weight7,100 to 8,300 lb
Crew2, side by side
Launch vehicleTitan II
Stage 1 thrust430,000 lb
Stage 2 thrust100,000 lb

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimePRE-LAUNCH
Day/Rev1/3
Page1-2
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

DID YOU KNOW?FLIGHT PLAN

NOTES

First Computer in Space

Gemini carried a 59-pound onboard computer with less memory than a short email — and flew orbital rendezvous with it.

GT-3 - first onboard computer on a crewed flight

The Sandwich Incident

John Young smuggled a corned beef sandwich aboard Gemini 3. Crumbs floated everywhere — and It came up in a House appropriations hearing.

Report: negative on crumbs

The Angry Alligator

When a docking target's nose cone jammed half-open, the crew radioed that it looked like an angry alligator.

The name stuck.

GT-9A - ATDA docking target
MissionGEMINI
EditionFINAL
Date1965 - 1966
Time
Day/Rev1/3
Page3-1
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Figure 3-1CABIN EQUIPMENT

NOTES
CABIN EQUIPMENT
Tap the drawing to enlarge

The front seat of a sports car, the engineers said, and they were not joking. Two ejection seats, two hatches, an instrument panel each and a center console they shared. Everything the crew touched for up to fourteen days is on this drawing.

  1. 1Crew hatch - one per man, hinged outward. The right hatch is the one Ed White stood up through on Gemini IV.
  2. 2Command pilot's instrument panel - attitude, altitude and the eight-ball flight director, on the left side.
  3. 3Center panel - the shared panel between the seats, including the computer keyboard.
  4. 4Attitude control handle - the stick that fired the thrusters, between the seats where either pilot could reach it.
  5. 5Ejection seats - Gemini had no escape tower. Below 70,000 feet the way out was straight up through the hatch.
  6. 6Secondary oxygen control handle - the backup supply, one per seat.
Cabin
Hatches2
Ejection seats2
Cabin pressure5.1 psi O2
Longest stay14 days (GT-7)

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimeORBIT
Day/Rev1/3
Page3-2
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Figure 3-5INSTRUMENT PANELS AND DISPLAYS

NOTES
INSTRUMENT PANELS AND DISPLAYS
Tap the drawing to enlarge

Every switch, gauge and circuit breaker in the Gemini cockpit, drawn flat. The left panel belongs to the command pilot, the right to the pilot, and the long center console between them carries the computer and the systems both men needed.

  1. 1Command pilot's main panel - flight director attitude indicator, altimeter, rate of descent and the event timer.
  2. 2Center console upper assembly - the Manual Data Insertion Unit: a keyboard and readout for the onboard computer, the first flown in space.
  3. 3Pilot's main panel - navigation and rendezvous displays, including the radar range and range-rate meters.
  4. 4Left switch and circuit breaker panel - electrical control for the command pilot's side.
  5. 5Attitude hand controller - pitch, roll and yaw in one grip, with maneuver thrusters on a second controller.
  6. 6Abort control - the handle that fired the ejection seats on the pad or triggered a high-altitude abort.
Displays
ComputerIBM, 59 lb
Memory4,096 words
Panels3 main
Crew stations2

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimeALL PHASES
Day/Rev1/3
Page3-21
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Section VISUMMARY FLIGHT PLAN

NOTES

Every crewed Gemini flight, in order. Durations are hours:minutes, the way the flight plan counts them.

FlightDateCrewDurationEvent
GT-3 23 Mar 1965 Grissom / Young 04:52 First crewed Gemini; first orbit change flown by a crew
GT-4 3 - 7 Jun 1965 McDivitt / White 97:56 First U.S. spacewalk - Ed White, about 20 minutes outside
GT-5 21 - 29 Aug 1965 Cooper / Conrad 190:55 Eight days in orbit; first fuel cells in a crewed spacecraft
GT-7 4 - 18 Dec 1965 Borman / Lovell 330:35 Fourteen-day endurance flight; target for GT-6A
GT-6A 15 - 16 Dec 1965 Schirra / Stafford 25:51 First rendezvous in space - held station with GT-7 to within a foot
GT-8 16 Mar 1966 Armstrong / Scott 10:41 First docking (Agena); stuck thruster forced an early landing
GT-9A 3 - 6 Jun 1966 Stafford / Cernan 72:21 The Angry Alligator; Cernan EVA 2h 07m
GT-10 18 - 21 Jul 1966 Young / Collins 70:47 Docked Agena used to boost to a 763 km record altitude
GT-11 12 - 15 Sep 1966 Conrad / Gordon 71:17 First-orbit rendezvous; 1,369 km altitude record; tethered flight
GT-12 11 - 15 Nov 1966 Lovell / Aldrin 94:35 Aldrin - 5h 30m of EVA; spacewalking finally solved

Gemini 1 and 2 flew uncrewed. Gemini 6 was renamed 6A after its Agena target was lost on launch.

MissionGEMINI
EditionFINAL
Date1965 - 1966
Time1965 - 1966
Day/Rev1/3
Page6-1
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Figure 13-1DOCKING SYSTEM

NOTES
DOCKING SYSTEM
Tap the drawing to enlarge

How two vehicles become one. Gemini's nose slid into the Agena's docking cone, three latches caught, and the cone drew the spacecraft in and locked it rigid. Neil Armstrong and Dave Scott did it first on Gemini VIII.

  1. 1Target vehicle - the Agena upper stage, launched separately and waiting in orbit.
  2. 2Docking cone - the funnel on the Agena that guided the nose in and absorbed the contact.
  3. 3Indexing bar - lined up with a notch in the cone so the two vehicles docked at the right roll angle.
  4. 4Mooring latches and latch hooks - three of them, caught by the Gemini nose and then pulled tight to rigidize.
  5. 5Rendezvous and Recovery section - the Gemini nose, with the radar inside and the parachutes behind it.
  6. 6Docking light - mounted on the capsule so the crew could see the cone in the dark.
Rendezvous and docking
First rendezvousGT-6A / GT-7
First dockingGT-8, 16 Mar 1966
TargetAgena GATV
Latches3

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimeRENDEZVOUS
Day/Rev1/3
Page13-2
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Figure 15-1AUGMENTED TARGET DOCKING ADAPTER

NOTES
AUGMENTED TARGET DOCKING ADAPTER
Tap the drawing to enlarge

The Angry Alligator, as drawn before it got its name. The ATDA was a docking cone on a short equipment section, built as a stand-in when Agenas were lost. On Gemini IX-A the shroud never came off, the jaws hung half open, and Tom Stafford radioed the description that stuck.

  1. 1Ascent shroud - meant to split and fall away after launch. On GT-9A it stayed on, held by lanyards that had been taped down.
  2. 2Docking cone - identical to the Agena's, so a Gemini could dock the same way.
  3. 3Equipment section - batteries, radio, radar transponder, and the attitude thrusters.
  4. 4Running lights - six of them, so the crew could find the target at night.
  5. 5Reaction Control System module - kept the ATDA pointed steady while Gemini approached.
  6. 6Launch configuration - the ATDA rode an Atlas, the same booster that carried Mercury.
ATDA
FlightGT-9A, 3 Jun 1966
BoosterAtlas
Shroudfailed to jettison
Dockednever
CrewStafford / Cernan

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimeGT-9A
Day/Rev1/3
Page15-4
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Section IVEVA PREPARATION AND EGRESS

NOTES

B. Test requirements - Gemini IV, 3 June 1965

Tick each item as you read it. This is the sequence Ed White and Jim McDivitt flew on the first American spacewalk; the equipment is in Section XVI of the manual.

Tap a box to check it off

Items complete 0/8GO FOR EVA
MissionGEMINI
EditionFINAL
Date1965 - 1966
Time04:18 - 04:58
Day/Rev1/3
Page4-10
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Figure 16-1TYPICAL USE OF EVA EQUIPMENT

NOTES
TYPICAL USE OF EVA EQUIPMENT
Tap the drawing to enlarge

The manual's own picture of a man outside. Chest pack, umbilical, hand-held maneuvering unit, gold visor - everything on this drawing was learned the hard way between Ed White's twenty minutes on Gemini IV and Buzz Aldrin's five and a half hours on Gemini XII.

  1. 1ELSS chest pack - the Extravehicular Life Support System. Oxygen, cooling and the warning lights, strapped to the chest.
  2. 2Hand-Held Maneuvering Unit - the zip gun. Short bursts of gas to move; it ran dry fast.
  3. 325-foot umbilical - oxygen hose, electrical line and tether in one bundle back to the cabin.
  4. 4Visor - a gold-coated sun visor over the pressure helmet; the sun outside is unfiltered.
  5. 5Gemini spacecraft - hatch open, the pilot's seat empty, the command pilot still strapped in.
EVA
First U.S. EVAGT-4, 3 Jun 1965
Umbilical25 ft
Most EVA on one flightGT-12, 5h 30m (three EVAs)
Total Gemini EVAabout 12 hrs

Source: NASA Project Gemini Familiarization Manual, SEDR 300 Vol. II, McDonnell, 1 July 1966.

MissionGEMINI
EditionFINAL
Date1965 - 1966
TimeEVA
Day/Rev1/3
Page16-2
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH
MCC-H

Section IABBREVIATIONS

NOTES
GETGround Elapsed Time - hours:minutes since liftoff
MSFNManned Space Flight Network - the ground stations; the double line on the ruler shows coverage
MCC-HMission Control Center, Houston
CAPCOMCapsule Communicator - the one voice on the ground that talks to the crew
CDR / PLTCommand pilot (left seat) and pilot (right seat)
GLVGemini Launch Vehicle - a modified Titan II missile
OAMSOrbit Attitude and Maneuvering System - the thrusters
RCSRe-entry Control System - thrusters for the ride home
R and RRendezvous and Recovery section - the nose: radar and parachutes
GATVGemini Agena Target Vehicle - the docking target
ATDAAugmented Target Docking Adapter - the Angry Alligator
EVAExtravehicular Activity - a spacewalk
ELSSExtravehicular Life Support System - the chest pack
HHMUHand-Held Maneuvering Unit - the zip gun
SEDRService Engineering Department Report - the McDonnell manual series this book is drawn from
GO / NO GOThe poll before every big step - every station must answer GO
MissionGEMINI
EditionFINAL
Date1965 - 1966
Time-
Day/Rev1/3
Page1-3
CKC Form 29 (May 65)FLIGHT PLANNING BRANCH