MODEL SPECIFICATION LIQUID PROPELLANT ROCKET ENGINE ROCKETDYNE MODEL YLR101-NA-15 (VERNIER)

reportActive / Technical Report | Accession Number: AD0409534 | Open PDF

Abstract:

Specification requirements for the YLR101-NA-15 rocket engine are reported. The engine is a calibrated, fixed-thrust bipropellant rocket engine with a nominal sea-level tank-fed rating of 525 pounds. The single thrust chamber shall be gimbal mounted, shall have an exhaust-nozzle expansion ratio of 5.61, and shall be regenera tively cooled using the fuel as the heat transfer medium.

Author(s):
Mccurdy, B. H.
Author Organization(s):
ROCKETDYNE CANOGA PARK CA
Pagination:
0147

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
53S
Contract/Grant Number(s):
AF 04(694)-58
Monitor Series:
USAF
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_4.6_Engineering; JCA_4.6.1_General Engineering; JCA_6_Net Centric; JCA_6.1.3_Switching and Routing; JCA_6.4.1_Secure Information Exchange; JCA_1_Force Support; JCA_6.1.1_Wired Transmission; JCA_1.3_Human Capital Management; JCA_6.1_Information Transport; JCA_1.3.2_Personnel Management; JCA_4.2_Supply; JCA_6.4_Information Assurance; JCA_4.3_Maintain; JCA_5_Command and Control; JCA_5.3_Planning; JCA_4.2.2_Inventory Management; JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*LIQUID PROPELLANT ROCKET ENGINES, *VERNIER ROCKET ENGINES, SPECIFICATIONS, SPECIFIC IMPULSE, THRUST CHAMBERS, BIPROPELLANTS
Field(s)/Group(s):
Liquid Propellant Rocket Engines
Keyword(s):
LR 101 ENGINES
Report Date:
1963 May 31