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Operational abort plan for the apollo 9 mission. volume 2: contingency deorbit
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1969 |
| Abstract | The Apollo 9 preflight nominal and contingency deorbit and reentry data are based on the Apollo 9 spacecraft operational trajectory. These data are designed not only as a contingency deorbit study, but also as a tool for flight control and flight dynamics SSR personnel use in simulation support and mission control. In addition to data for the mass properties, data are presented for GO - NO-GO area and general reentry studies for the nominal reentry into the prime Atlantic recovery area, 151-1. Volume I of this document gives the abort data for the launch phase. |
| File Size | 3000737 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19740072948 |
| Archival Resource Key | ark:/13960/t0ft9980t |
| Language | English |
| Publisher Date | 1969-02-13 |
| Access Restriction | Open |
| Subject Keyword | Mission Planning Space Shuttles Low Earth Orbits Nasa Programs Piggyback Systems Recoverable Launch Vehicles Reusable Spacecraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
