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Accession Number:
AD0423340
Title:
DEVELOPMENT OF DOWNRATED ATLAS YLR101-NA-15 VERNIER ENGINE
Corporate Author:
ROCKETDYNE CANOGA PARK CA
Report Date:
1963-11-08
Abstract:
Presented is a summary of test results from a program to develop the YLR101-NA-15 vernier engine. The program was completed in three phases 1 Downrating the tank-fed thrust of the YLR101-NA-13 vernier from 830 pounds to 525 pounds, 2 modifying and repackaging the 525pound-thrust vernier into the YLR101-NA-15 configuration, and 3 developing a modified vernier injector to minimize a thrust chamber erosion problem which occurred at the 525-pound-thrust level.
Descriptive Note:
Final rept., Oct 1962-Oct 1963
Pages:
0168
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
AF 04(695)-306
File Size:
9.21MB
