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Accession Number:
AD0375709
Title:
COMPARISON OF ADVANCED RAMJET ENGINES.
Corporate Author:
NAVAL ORDNANCE TEST STATION CHINA LAKE CA
Report Date:
1965-01-01
Abstract:
The technological status of a boron-slurry and the low-volume ramjet engines was reviewed. Engine performance maps including parametric variations of the critical assumptions were developed. Numerous preliminary designs of the ARM-II missile system utilizing each propulsion system were made. The range performance for a low-altitude, high-speed trajectory was calculated for each design and its parametric variations. The results show the boron-slurry engine offers a substantial range performance advantage over the low-volume ramjet engine for both the weight and volume limited cases.
Descriptive Note:
Technical publication,
Pages:
0040
File Size:
0.00MB
