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.

Subject Categories:

  • Air- and Space-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE