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Shuttle/agena study. annex a: ascent agena configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1972 |
| Description | Details are presented on the Agena rocket vehicle description, vehicle interfaces, environmental constraints and test requirements, software programs, and ground support equipment. The basic design concept for the Ascent Agena is identified as optimization of reliability, flexibility, performance capabilities, and economy through the use of tested and flight-proven hardware. The development history of the Agenas A, B, and D is outlined and space applications are described. |
| File Size | 171787806 |
| Page Count | 194 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720013179 |
| Archival Resource Key | ark:/13960/t70w37s3g |
| Language | English |
| Publisher Date | 1972-02-15 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Computer Programming Ascent Propulsion Systems Space Shuttles Agena Rocket Vehicles Space Tugs Ground Support Equipment Spacecraft Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |