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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
19670059068
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kelley, J. H.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Space Vehicles
Accession Number
67A37797
Distribution Limits
Public
Copyright
Other
Keywords
SPECIFIC IMPULSE
SPACECRAFT MANEUVER
VELOCITY ERROR
HYDRAZINE ENGINE /NIMPHE/
BURNING RATE
MARINER IV SPACE PROBE
LOW THRUST PROPULSION

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