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Accession Number:
ADA056077
Title:
Combustion Properties of High-Density Fuels.
Corporate Author:
MARTIN MARIETTA LABS BALTIMORE MD
Report Date:
1977-01-01
Abstract:
For tactical systems operating within the atmosphere, ramjet propulsion offers significant advantages over conventional rocket propulsion systems i.e., those which carry both fuel and oxidizer. The principal advantages -- increased range or greater payload at fixed range -- result from the intrinsic high specific impulse Isp associated with ramjets, which only need to carry fuel the oxidizer being obtained from the atmosphere for their propulsion.
Descriptive Note:
Quarterly rept. no. 1, 1 Nov 76-31 Jan 77,
Pages:
0018
Contract Number:
N00019-76-C-0683
File Size:
6.23MB
