Apollo 1 Spacecraft History
Event |
Date |
Fabrication of spacecraft
012 at North American Aviation, |
Aug 1964 |
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Basic structure completed. |
Sept 1965 |
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Installation and final assembly of subsystems completed. Critical design reviews completed. Checkout of all subsystems initiated, followed by integrated testing of all spacecraft subsystems. |
Mar 1966 |
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Customer acceptance readiness review completed. NASA issued certificate of flightworthiness and authorized spacecraft to be shipped to KSC. |
Aug 1966 |
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Command module received at KSC. |
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CM-012 mated with service module in altitude chamber. Alignment, subsystems and system certification tests and functional checks performed. |
Sep 1966 |
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First combined systems tests completed. |
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Design certification document issued which certified design as flightworthy, pending satisfactory resolution of open items. |
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First manned test at sea level pressure to verify total spacecraft system operation completed. |
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Unmanned test at altitude pressures using oxygen to verify spacecraft system operation. |
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Manned test with flight crew completed. |
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Second manned altitude test with backup crew initiated, but discontinued when failure occurred in oxygen system regulator in spacecraft environmental control system. Regulator removed and found to have design deficiency. |
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Apollo program director conducted recertification review which closed out majority of open items remaining from previous reviews. |
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Sea level and unmanned altitude tests completed. |
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Manned altitude test with backup flight crew completed. |
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Command module removed from altitude chamber. |
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Spacecraft mated to launch vehicle at Cape Kennedy Launch Complex 34. Various tests and equipment installations and replacements performed. |
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