DEVELOPMENT OF AN ELASTOMERIC SEAL FOR OMNIAXIAL MOVABLE NOZZLES (LOCKSEAL).

reportActive / Technical Report | Accession Number: AD0373032 | Need Help?

Abstract:

The technical effort of the development of an elastomeric seal for omniaxial movable nozzles, is presented. The technical effort in this period included 1 complete analysis of the elastomeric pads and metallic reinforcements in the seal, 2 bench tests on four development seals, and 3 rocket motor firings on three Lockseal TVC systems. The results of this effort are reviewed in this report.

Author(s):
No Author(s) Identified
Author Organization(s):
LOCKHEED PROPULSION CO REDLANDS CALIF
Descriptive Note:
Final rept. 4 Jan 65-31 Mar 66.
Annotation:
Development of an elastomeric seal for omniaxial movable nozzles.
Pagination:
0177

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
LPC-689-F, AFRPL-TR-66-112
Contract/Grant Number(s):
AF 04(611)-10537
Project Number(s):
AF-3059
Monitor Series:
TR-66-112
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Weapons Technologies
Descriptor(s):
(*ROCKET NOZZLES, *MOVABLE NOZZLES), (*THRUST VECTOR CONTROL SYSTEMS, MOVABLE NOZZLES), *SOLID PROPELLANT ROCKET ENGINES), O RINGS, SEALS, ELASTOMERS, SHEAR STRESSES, COMBUSTION CHAMBERS, PRESSURE, EROSION, DEFLECTION, STRUCTURAL PROPERTIES, FORCE(MECHANICS), TORQUE, REINFORCING MATERIALS, DEFORMATION, LOAD DISTRIBUTION (U) BUCKLING, SECOND STAGE MOTORS, SANDWICH CONSTRUCTION
Field(s)/Group(s):
Solid Propellant Rocket Engines
Keyword(s):
COLUMNS(STRUCTURAL), MINUTEMAN, M 56 MOTORS
Report Date:
1966 Apr 01