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Rectilinear display gives acceleration load factor and velocity informationSpacecraft entry monitoring system /EMS/ gives a rectilinear display of acceleration load factor and velocity information. This allows an astronaut to respond with manual spacecraft attitude corrective maneuver commands.
Document ID
19670000248
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Frank, A. J.
Johnson, B. C.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Electronic Components And Circuits
Report/Patent Number
MSC-1045
Report Number: MSC-1045
Accession Number
67B10248
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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