FORTE spacecraft vibration mitigation. Final report
This report documents work that was performed by CSA Engineering, Inc., for Los Alamos National Laboratory (LANL), to reduce vibrations of the FORTE spacecraft by retrofitting damped structural components into the spacecraft structure. The technical objective of the work was reduction of response at the location of payload components when the structure is subjected to the dynamic loading associated with launch and proto-qualification testing. FORTE is a small satellite that will be placed in orbit in 1996. The structure weighs approximately 425 lb, and is roughly 80 inches high and 40 inches in diameter. It was developed and built by LANL in conjunction with Sandia National Laboratories Albuquerque for the United States Department of Energy. The FORTE primary structure was fabricated primarily with graphite epoxy, using aluminum honeycomb core material for equipment decks and solar panel substrates. Equipment decks were bonded and bolted through aluminum mounting blocks to adjoining structure.
- Research Organization:
- Los Alamos National Lab., NM (United States); CSA Engineering, Inc., Palo Alto, CA (United States)
- Sponsoring Organization:
- USDOE, Washington, DC (United States)
- DOE Contract Number:
- W-7405-ENG-36
- OSTI ID:
- 484535
- Report Number(s):
- LA-SUB--96-109; ON: DE97007543
- Country of Publication:
- United States
- Language:
- English
Similar Records
Viscoelastic struts for vibration mitigation of FORTE
Development of a new class of satellites: a composite lightweight affordable spacecraft structure
Development of a composite satellite structure for FORTE
Technical Report
·
Wed May 01 00:00:00 EDT 1996
·
OSTI ID:226056
Development of a new class of satellites: a composite lightweight affordable spacecraft structure
Conference
·
Sat Jun 01 00:00:00 EDT 1996
·
OSTI ID:244505
Development of a composite satellite structure for FORTE
Conference
·
Fri Mar 31 23:00:00 EST 1995
·
OSTI ID:62626