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Chemical propulsion - The old and the new challengesThe historical background concerning the application of liquid propellant rockets is considered. Progress to date in chemical liquid propellant rocket engines can be summarized as an increase in performance through the use of more energetic propellant combinations and increased combustion pressure. New advances regarding liquid propellant rocket engines are related to the requirement for reusability in connection with the development of the Space Shuttle.
Document ID
19740056623
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mccarty, J. P.
Lombardo, J. A.
(NASA Marshall Space Flight Center Astronautics Laboratory, Huntsville, Ala., United States)
Date Acquired
August 7, 2013
Publication Date
December 1, 1973
Publication Information
Publication: AIAA Student Journal
Volume: 11
Subject Category
Propulsion Systems
Accession Number
74A39373
Distribution Limits
Public
Copyright
Other

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