NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Application of blast wave theory to explosive propulsionAn analysis was carried out by using blast wave theory to delineate the important aspects of detonating explosives in nozzles, such as flow and wave phenomena, characteristic length and time scales, and the parameters on which the specific impulse is dependent. The propulsive system utilizes the momentum of the ambient gas set into motion in the nozzle by the explosion. A somewhat simplified model was considered for the situation where the mass of ambient gas in the nozzle is much greater than the mass of gas produced in the explosion, a condition of interest for dense atmospheres, e.g., near the surface of Venus. Instantaneous detonation and energy release was presumed to occur at the apex of a conical nozzle, and the shock wave generated by the explosion was taken to propagate as a spherical wave, thereby setting the ambient gas in the nozzle into one-dimensional radially outward motion.
Document ID
19750057805
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Back, L. H.
(California Institute of Technology, Jet Propulsion Laboratory, Propulsion Research and Advanced Concepts Section, Pasadena Calif., United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1975
Publication Information
Publication: Acta Astronautica
Volume: 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
75A41877
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available