Accession Number:

ADA279923

Title:

Shock and Vibration Testing of a Rocket-Boosted RF Decoy

Descriptive Note:

Final rept.,

Corporate Author:

NAVAL RESEARCH LAB WASHINGTON DC

Personal Author(s):

• Walden, Ronald B.
• Page, Gregory S.

Report Date:

1994-05-18

Pagination or Media Count:

17.0

Abstract:

In order to evaluate the survivability of the RF payload, associated avionics, and structural integrity of the FLYRT RF decoy, a series of vibration and shock tests were performed. Presented are the experiments and their subsequent results

Descriptors:

• *BOOSTER ROCKET ENGINES
• AVIONICS
• VIBRATION
• ACCELERATION
• DECOYS
• SHOCK TESTS

Subject Categories:

• Mechanics
• Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE