Timeline diagram showing boxes labeled GYMEX, CNT, ANT, ASC, PRE, TAN, N/GHT, CDO, HAW

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FIG. 1 - Labeled diagram of Gemini spacecraft showing components including rendezvous guidance & recovery system, re-entry capsule, adapter section, separation point, oxidizer tank, equipment bay, fuel tank, Stage II engine thrust chamber, Stage I engine gimbal point, and Stage I engine thrust chambers. Equipment bay contains: Batteries, Malfunction detection system (MDS) units, Range safety command control set, Programmer, Three-axis reference system (TARS), Reaction control system (RCS), Autopilot, Instrumentation and telemetry system.

Abort procedures diagram showing three modes with altitude and time parameters, including velocity markers at 29,700 FPS and 78,000 FT, with delayed mode and retrofire sequences

GEMINI LAUNCH SEQUENCE - Figure 20 showing altitude vs range trajectory with mission events

GEMINI PARACHUTE LANDING SEQUENCE showing descent stages from 30,000 feet to touchdown with labeled parachute deployments