Multi-axis whole-spacecraft vibration isolation for small launch vehicles

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4331, Issue , 2001, Pages 153-161

  Johnson, C D ^a   Wilke, P S ^a   Darling, K R ^a  

^a CSA ENGINEERING   (United States)

Author keywords

Launch load attenuation; Softride; Spacecraft isolation; Suppression; Vibration isolation

Indexed keywords

AERODYNAMIC LOADS; ALGORITHMS; SATELLITES; TELEMETERING; VIBRATION CONTROL;

LAUNCH VEHICLES; VIBRATION ISOLATION SYSTEMS;

LAUNCHING;

EID: 0034852222     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.432699     Document Type: Conference Paper

References (1)

1. Orbital Suborbital Program (OSP) "Minotaur" space launch vehicle: Low cost space lift for small satellites using surplus minuteman motors