NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Minimum thrust levels for spinning drag-free satellitesA drag-free satellite, which contains an internal unsupported proof mass, is shielded from external forces such as solar pressure. Thrustors force the satellite to follow the proof mass and hence the satellite follows an almost purely gravitational orbit. The dominant internal disturbing force is the mass attraction of the satellite on the proof mass. Spinning the satellite reduces this force and it has been investigated what the size of the thrustors must be in this case. This size is much smaller than originally thought. Its impact on some other features is shown.
Document ID
19760032808
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Olsder, G. J.
(Technische Hogeschool Twente Enschede, Netherlands)
Powell, J. D.
(Stanford University Stanford, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Publication Information
Publication: Automatica
Volume: 11
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76A15774
Funding Number(s)
CONTRACT_GRANT: NAS5-21684
CONTRACT_GRANT: ZWO-S61-25
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available