Passive and active launch vibration studies in the LVIS program

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 3327, Issue , 1998, Pages 411-422

  Edberg, Donald L ^a   Bartos, Bruce ^a   Goodding, James ^a   Wilke, Paul ^a   Davis, Torey ^a  

^a BOEING COMPANY   (United States)

Author keywords

Attenuation; Launch vehicle; Payload attach fitting; Vibration isolation

Indexed keywords

ATTENUATION; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; SPACECRAFT; STIFFNESS; VIBRATION MEASUREMENT;

LAUNCH VIBRATION ISOLATION SYSTEM (LVIS);

LAUNCHING;

EID: 0032403775     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.310703     Document Type: Conference Paper

References (2)

1. On the development of a launch vibration isolation system