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NASA Project Gemini Long Range And Modified Configs Manual Vol 1

NASA Project Gemini Long Range and Modified Configs Manual Vol 1 Long Range and Modified Configurations - Sections 1 through 12, except Section 8. Section 8 is contained in a supplement to this manual, volume 2. Sep 30, 1965, 485 pages by the McDonnell Aircraft Company The Gemini spacecraft is maneuverable within its orbit and will rendezvous with and connect to a second orbiting vehicle. Depending upon the specific mission objective, it can stay in orbit up to fourteen days. Finally, upon re-entry, the re-entry portion of the spacecraft can be controlled in a relatively conventional landing. The modified and long range configurations of the spacecraft, however, with which this manual is specifically concerned, perform a variety of missions. SECTION INDEX SECTION I SPACECRAFT MISSION SECTION II MAJOR STRUCTURAL ASSEMBLY SECTION III CABIN INTERIOR ARRANGEMENT SECTION IV SEQUENCE SYSTEM SECTION V ELECTRICAL POWER SYSTEM SECTION VI ENVIRONMENTAL CONTROL SYSTEM SECTION V COOLING SECTION VIII GUIDANCE AND CONTROL SYSTEM (all in Volume 2) SECTION IX COMMUNICATIONS SYSTEM SECTION X INSTRUMENTATION AND RECORDING SYSTEM SECTION XI PYROTECHNICS AND RETROGRADE ROCKET SECTION XII LANDING SYSTE

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