RECOVERY OF HIGH-PERFORMANCE RE-ENTRY VEHICLES BY DRAG BRAKES PLUS PARACHUTES

被引:0
|
作者
STECK, HJ
BERMAN, RJ
BLANCO, TT
机构
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:746 / &
相关论文
共 50 条
  • [11] HIGH-PERFORMANCE PARACHUTES
    PETERSON, CW
    SCIENTIFIC AMERICAN, 1990, 262 (05) : 108 - &
  • [12] Millimeterwave communications for atmospheric re-entry vehicles
    Christopher, P
    WIRELESS TECHNOLOGIES AND SYSTEMS: MILLIMETER-WAVE AND OPTICAL, 1998, 3232 : 21 - 32
  • [13] THE SEARCH FOR OPTIMUM CONFIGURATIONS FOR RE-ENTRY VEHICLES
    LIN, TC
    GRABOWSKY, WR
    YELMGREN, KE
    JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (02) : 142 - 149
  • [14] Optimal trajectories for maneuvering re-entry vehicles
    Undurti, Aditya
    Proulx, Ronald J.
    Shearer, James A.
    Setturlund, Roy H.
    ASTRODYNAMICS 2007, PTS I-III, 2008, 129 : 879 - +
  • [15] EFFECT OF MAGNETIC DRAG ON RE-ENTRY BODY HEATING
    PHILLIPS, RL
    ARS JOURNAL, 1961, 31 (05): : 672 - 674
  • [16] Aerodynamics and Aerothermodynamics of undulated re-entry vehicles
    Kaushikh, K.
    Arunvinthan, S.
    Pillai, S. Nadaraja
    ACTA ASTRONAUTICA, 2018, 142 : 95 - 102
  • [17] Aerodynamic design of a re-entry capsule for high-speed manned re-entry
    Chen, Bingyan
    Zhan, Huiling
    Zhou, Weijiang
    ACTA ASTRONAUTICA, 2015, 106 : 160 - 169
  • [18] Design criteria for low risk re-entry vehicles
    Monti, R
    Pezzella, G
    Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles, 2004, 563 : 197 - 204
  • [19] Heat alleviation studies on hypersonic re-entry vehicles
    1673, Cambridge University Press (122):
  • [20] AEROTHERMODYNAMIC CHARACTERISTICS OF SLENDER ABLATING RE-ENTRY VEHICLES
    TIMMER, HG
    ARNE, CL
    STOKES, TR
    TANG, HH
    JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (04) : 373 - &