Persistent re-entry vehicle roll resonance-Reference-Cited by-同舟云学术

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Persistent re-entry vehicle roll resonance

Published:1966-01-24 Issue: Volume: Page:
ISSN:
Container-title:3rd and 4th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

PETTUS J.¹

Affiliation:

1. GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., RE-ENTRY SYSTEMS DEPT., PHILADELPHIA, PA.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1966-49

Reference20 articles.

1. Bdy-Axis System", NACATN 3737,dated 1956. 4. Herburt, P. andMerchant,D. "The Importance of Pitch-Yaw Rolling

2. Momentson Skylark Vehicle", Royal AircraftEstablishment, TNG.W. 583, dated 1961. U.K. 5. Glover, L. "Effects On Roll Rateof Mass and Aerodynamic Asymmetries

3. G.E. ARO Memo 128,dated 1965.

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Missile and spacecraft coning instabilities;Astrodynamics Conference;1992-08-10

2. Effects of unsymmetrical stability derivative characteristics on re-entry vehicle transient angular motion;Journal of Spacecraft and Rockets;1976-02

3. Low-altitude roll behavior of entry vehicles with mass asymmetries;Journal of Spacecraft and Rockets;1975-09

4. Angle-of-attack control of drag for slender reentry vehicle recovery;5th Aerodynamic Deceleration Systems Conference;1975-08-16

5. Angle-of-Attack Control of Spinning Missiles;Journal of Spacecraft and Rockets;1975-04

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