MINIATURE MAGNETIC SPIN RATE SENSOR FOR SOUNDING ROCKETS

被引:0
|
作者
JENKINS, GJ [1 ]
LUND, FP [1 ]
机构
[1] UNIV SOUTHAMPTON,PHYS DEPT,SOUTHAMPTON SO9 5NH,ENGLAND
来源
关键词
D O I
10.1088/0022-3735/6/7/016
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
引用
收藏
页码:637 / 638
页数:2
相关论文
共 50 条
  • [31] SYMPOSIUM ON SOUNDING ROCKETS AND EXPERIMENTAL RESULTS
    不详
    SPACEFLIGHT, 1972, 14 (01): : 34 - &
  • [32] A GPS RECEIVER FOR USE IN SOUNDING ROCKETS
    Mota, Francisco
    Albuquerque, Glauberto
    Raposo, Tullio
    20TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH, 2011, 700 : 173 - 177
  • [33] TECHNICAL ASPECTS OF THE BRAZILIAN SOUNDING ROCKETS
    Correa Junior, Flavio de Azevedo
    da Silva Mello Junior, Alberto Walter
    PROCEEDINGS OF THE 21ST ESA SYMPOSIUM ON EUROPEAN ROCKET & BALLOON PROGRAMMES AND RESEARCH, 2013, 721 : 125 - 131
  • [34] SOUNDING ROCKETS SHOT FROM THE SHUTTLE
    CRUDDACE, R
    FRITZ, G
    GLAAB, J
    SHREWSBERRY, D
    AEROSPACE AMERICA, 1985, 23 (07) : 74 - 76
  • [35] Image processing based horizon sensor for estimating the orientation of sounding rockets, launch vehicles and spacecraft
    Benjamin Braun
    Jochen Barf
    CEAS Space Journal, 2023, 15 : 509 - 533
  • [36] Image processing based horizon sensor for estimating the orientation of sounding rockets, launch vehicles and spacecraft
    Braun, Benjamin
    Barf, Jochen
    CEAS SPACE JOURNAL, 2023, 15 (03) : 509 - 533
  • [37] Digital attitude control for NASA sounding rockets
    Martinez, C
    MISSIONS TO THE SUN II, 1998, 3442 : 157 - 165
  • [38] Microgravity experiments in sounding rockets, spacelab and EURECA
    不详
    CAPILLARY SURFACES, 2002, 178 : 323 - 359
  • [39] An overview of the NASA Sounding Rockets and Balloon Programs
    Flowers, BJ
    Needleman, HC
    14TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH, 1999, 437 : 65 - 72
  • [40] "Baby" Rocket: The Eve of Sounding Rockets in Japan
    Matogawa, Yasunori
    HISTORY OF ROCKETRY AND ASTRONAUTICS, 2010, 32 : 361 - 376