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Throttleable thruster system design, fabrication and test verificationThrottleable thrustor system for Mars soft landing, selecting catalytic decomposition engine from system weight and performance studies
Document ID
19700057433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kenny, R. J.
Reeves, D. F.
Date Acquired
August 5, 2013
Publication Date
June 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 70-652
Report Number: AIAA PAPER 70-652
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH
Location: SAN DIEGO, CA
Start Date: June 15, 1970
End Date: June 19, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A33549
Funding Number(s)
CONTRACT_GRANT: JPL-952344
Distribution Limits
Public
Copyright
Other

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