Whole-spacecraft shock isolation system

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4697, Issue , 2002, Pages 1-8

  Johnson, Conor D ^a   Wilke, Paul S ^a  

^a CSA ENGINEERING   (United States)

Author keywords

Launch Environment; Shock; Shock Isolation; Spacecraft Vibration Protection

Indexed keywords

AVIONICS; COMPUTER SIMULATION; DATA REDUCTION; DYNAMIC LOADS; EQUIPMENT TESTING; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; PNEUMATIC CONTROL; SPACECRAFT INSTRUMENTS; VIBRATION CONTROL;

SPACECRAFT VIBRATION PROTECTION; WHOLE-SPACECRAFT VIBRATION ISOLATION SYSTEMS;

SHOCK ABSORBERS;

EID: 0036380316     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.472644     Document Type: Conference Paper

References (3)

1. Paul S. Wilke, Conor D. Johnson, Patrick J. Gosserode, Dino Sciulli, "Whole-Spacecraft Vibration Isolation on Small Launch Vehicles", Proceedings of the Smart Materials and Structures, Damping and Isolation, Vol 3989, pgs 440-451, March 6-8, 2000, Newport Beach, CA
2. Conor D. Johnson, Paul S. Wilke, Kenneth R. Darling, "Multi-axis whole-spacecraft vibration isolation for small launch vehicles", Proceedings of the Smart Materials and Structures, Damping and Isolation, Vol 4331, pgs 153161, March 5-7, 2001, Newport Beach, CA
3. Conor D. Johnson, Paul S. Wilke, "Recent Launches using the SoftRide Whole-Spacecraft Vibration Isolation System", Proceedings of the AIAA Space 2001 Conference, August 2001, Albuquerque, NM