NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
High stability deployable boomMeaningful magnetic field vector measurements in space require accurate placement of a magnetometer beyond the magnetic fields of a spacecraft. The design and development of a deployable boom is described which ensures accurate deployment of an instrument package and maintains high stability after extension.
Document ID
19760021198
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, G. A. (Fairchild Space and Electronics Co. Germantown, MD, United States)
Berry, T. G. (Fairchild Space and Electronics Co. Germantown, MD, United States)
Dibiasi, L. (Fairchild Space and Electronics Co. Germantown, MD, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N28286
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760021184Collected WorksTenth Aerospace Mechanisms Symposium
No Preview Available