NASA/SP-8098, Effects of structural flexibility on entry vehicle control systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance), NASA (Washington, DC, United States), June,1972, pp. 68, Format(s): PDF 4254k |
Control system/structure interactions of space vehicles during planetary and earth entry were investigated with principal emphasis on atmospheric entry and aerodynamic deceleration to subsonic speeds.
| Keywords: | space vehicles, atmospheric entry, flexibility, reentry vehicles, spacecraft control, control equipment, systems engineering |
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| CASI Document ID Number: | 72N29870 |
| Subjects: | Engineering: Structural Mechanics: Structural Tests and Reliability Astronautics: Launch Vehicles And Launch Operations: Reentry Vehicles |
| ID Code: | 128 |
| Deposited On: | 23 May 2002 |