DEVELOPMENT OF GENERATOR, PROPELLANT ACTUATED, XM14.

reportActive / Technical Report | Accession Number: AD0613164 | Need Help?

Abstract:

A dual gas generator was developed to provide a source of pneumatic power for operating the pre-ejection system for the B58 escape capsule. The gas produced operates a series of leg-positioning and torso-retracting mechanisms and ultimately releases and closes the capsule doors. A high temperature-resistant propellant and igniter were used to meet extended storage and operating requirements at 200F. The dual generator permits use of one charge to enclose the crew member in an emergency. If the emergency passes without ejection, the second generator can be fired to operate the system should this become necessary. A special shift valve arrangement, integral trap, and rupture assembly make for a high degree of reliability and safety. The results of evaluation tests showed the dual gas generator XM14 capable of meeting the design requirements. Author

Author(s):
Stiefel, Ludwig ; Catrambone, George P. ; Sutter, Raymond C.
Author Organization(s):
FRANKFORD ARSENAL PHILADELPHIA PA RESEARCH AND DEVELOPMENT DIRECTORATE
Descriptive Note:
Technical research rept.,
Supplementary Note:
Available copy will not permit fully legible reproduction. Reproduction will be made if requested by users of DDC. Copy is available for public sale.
Annotation:
Development of propellant actuated gas generator for B-58 pre-ejection system.
Pagination:
0051

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
R-1751
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
PROPELLANTS, BURNING RATE, CARTRIDGES(PAD), PNEUMATIC EQUIPMENT, BALLISTICS, HYDROSTATICS, VIBRATION, PERFORMANCE(ENGINEERING), DROP TESTS, SPECIFICATIONS
Keyword(s):
B 58 AIRCRAFT
Report Date:
1965 Feb 01