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Mariner IV midcourse propulsion system impulse and accuracy prediction.Mariner IV midcourse 50-lb thrust pressure- controlled monopropellant hydrazine propellant system, predicting impulse and velocity error as function of burn time
Document ID
19670033553
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelley, J. H.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-948
JPL-TR-32-1194
Report Number: AIAA PAPER 66-948
Report Number: JPL-TR-32-1194
Accession Number
67A12282
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other
Keywords
MARINER IV SPACE PROBE
SPACECRAFT MANEUVER
HYDRAZINE ENGINE /NIMPHE/
SPECIFIC IMPULSE
BURNING RATE
LOW THRUST PROPULSION
VELOCITY ERROR

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