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Dynamic Environment of the Ranger Spacecraft I Through IX (Final Report)The dynamic environment of the Ranger spacecraft (I through IX)during the launch portion of flight is defined in this Report. Flight data from each of nine spacecraft launches have been reviewed and are included. The environments receiving emphasis herein include liftoff acoustics, liftoff and transonic vibration, and the transient vibrations of the various pyrotechnic and staging events in the launch sequence. The systems for data acquisition and analysis are briefly described. In addition, post-flight comparison of flight data and ground test specification levels is made, and the dynamic test program is briefly discussed.
Document ID
19660017577
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Wiksten, D. B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 1, 1966
Subject Category
Launch Vehicles And Launch Operations
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-75273
JPL-TR-32-909
Report Number: NASA-CR-75273
Report Number: JPL-TR-32-909
Accession Number
66N26867
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK
RANGER PROJECT
ACOUSTICS
LAUNCHING
VIBRATION
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