Recent launches using the SoftRide whole-spacecraft vibration isolation system

AIAA Space 2001 Conference and Exposition

Volumn , Issue , 2001, Pages

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

^a CSA ENGINEERING   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LAUNCH VEHICLES; LAUNCHING; ORBITS; SMALL SATELLITES;

ACOUSTIC LOADS; AXIAL ISOLATION; COUPLED LOADS ANALYSIS; ISOLATION SYSTEMS; ORTHOGONAL AXES; SMALL LAUNCH VEHICLES; VIBRATION ISOLATIONS; WHOLE SPACECRAFT VIBRATION ISOLATIONS;

VIBRATIONS (MECHANICAL);

EID: 85088344165     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4708     Document Type: Conference Paper

References (3)

1. Orbital Sciences Corporation, "Taurus Launch System Payload User's Guide", Release 3.0, September, 1999
2. Orbital Sciences Corporation, "Minotaur Payload User's Guide", Draft version, April 26, 2001
3. Schoneman, S., Buckley, S., et al, "Orbital Suborbital Program (OSP)" Minotaur "Space Launch Vehicle: Low Cost Space Lift For Small Satellites Using Surplus Minuteman Motors", AIAA Paper AIAA-2000-5068, AIAA Space 2000 Conference, September 19-21, 2000, Long Beach, CA.