Test Report, HAWK Launcher Shock Absorber Spring, Part Number 9089062, Spring Rate and Residual Deflection Tests.

reportActive / Technical Report | Accession Number: ADA105804 | Open PDF

Abstract:

This report presents a description of the tests performed to determine the spring dimensional and loadcompression characteristics of the Hawk launcher shock absorber spring and their results. Author

Author(s):
Alston, John D.
Author Organization(s):
ARMY MISSILE COMMAND REDSTONE ARSENAL AL GROUND EQUIPMENT AND MISSILE STRUCTURES DIRECTORATE
Descriptive Note:
Technical rept.,
Pagination:
0016

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
DRSMI/RL-81-9-TR, SBI-AD-E950 159
Monitor Series:
AD-E950 159
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_5_Command and Control; JCA_6.4.1_Secure Information Exchange; JCA_1.2.5_Lessons Learned
Communities of Interest:
Weapons Technologies
Descriptor(s):
*GUIDED MISSILE LAUNCHERS, *HELICAL SPRINGS, *SHOCK ABSORBERS, COMPRESSION, PISTONS, PERFORMANCE TESTS, LOADS(FORCES), DEFLECTION, TEST METHODS, TEST EQUIPMENT, SURFACE TO AIR MISSILES, FORCE(MECHANICS)
Field(s)/Group(s):
Guided Missile Launching and Basing Support
Keyword(s):
Hawk missiles
Report Date:
1981 Feb 26