Accession Number:
ADA037067
Title:
Evaluation of the Harpoon Missile Shock Environment During Ejection Launch by Aircraft Launchers.
Descriptive Note:
Final rept. Jul 73-Nov 75,
Corporate Author:
BOLT BERANEK AND NEWMAN INC CANOGA PARKCA
Personal Author(s):
Report Date:
1977-02-01
Pagination or Media Count:
43.0
Abstract:
A series of ground launch ejections of a Harpoon missile were performed to establish and evaluate the Harpoon ejection shock environment. The acceleration response of the missile was measured at 30 locations during various ejections from an MAU-9AA and an Aero-7A-1 rack. The data were reduced to acceleration shock spectra covering a frequency range from 100 to 10 000 Hz. The results of the study produced considerable information concerning launch ejection shock environments of general interest.
Descriptors:
Subject Categories:
- Air- and Space-Launched Guided Missiles