NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
End-mass instrumentation for the first SEDS/Delta II missionThe dynamics instrumentation is described which will be flown in the end-mass of the first tethered satellite to be deployed from a Delta II launch vehicle with the SEDS (Small Expendable Deployer System) low-tension deployer. Transducers, signal conditioning, power supply design, data acquisition procedures and data recovery plans are discussed. The effects of temperature variations and other potential error sources are considered.
Document ID
19900035172
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deloach, R. (NASA Langley Research Center Hampton, VA, United States)
Diamond, J. (NASA Langley Research Center Hampton, VA, United States)
Finley, T. (NASA Langley Research Center Hampton, VA, United States)
Rhew, R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 90-0537
Accession Number
90A22227
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available