NASA/SP-8001-REV, Cole Jr.*, H.A. and Erickson*, A.L. and Rainey**, A.G., Buffeting during atmospheric ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Ames Research, **Langley Research Center, May,1964, pp. 19, Format(s): PDF 1437k |
Aeroelastic spacecraft design to minimize buffeting during atmospheric ascent.
| Keywords: | space vehicles, ascent, buffeting, spacecraft, design, spacecraft, stability, aeroelasticity, earth atmosphere, optimization |
|---|---|
| CASI Document ID Number: | 71N20473 |
| Subjects: | Astronautics: Spacecraft Design, Testing And Performance: Spacecraft Attitude Control And Stabilization |
| ID Code: | 27 |
| Deposited On: | 16 July 2002 |