Accession Number:

ADA135895

Title:

AQM-81A Firebolt.

Descriptive Note:

Corporate Author:

TACTICAL AIR COMMAND LANGLEY AFB VA

Personal Author(s):

Report Date:

1983-10-21

Pagination or Media Count:

5.0

Abstract:

Supersonic subscale aerial targets are required for employment in weapons system development, test and evaluation, and training to simulate high performance aircraft and missiles. As a result of extensive studies by the Air Force and Navy and successful completion of advanced development, the AQM-81A Firebolt has been selected at the most cost effective solution to satisfy projected high altitude supersonic requirements. The AQM-81A Firebolt vehicle is 216 inches long and 13 inches in diameter. The propulsion system uses a solid propellant with a liquid oxidizer catalyst. The vehicle contains a parachute recovery system to allow midair retrieval as the primary recovery procedure and a flotation system to allow water recovery. A Programmable Radar Augmentation System PRAS provides in the forward hemisphere 10 to -60 sq m degrees in elevation. The Scalar Scoring System SSS provides missiles miss distance information throughout 90 percent of the scoring volume described by a 150-foot sphere centered on the target. The purpose of this project is to support AFOTEC in the IOTE of the AQM-81A Firebolt system. The purpose of the AQM-81A IOTE is to evaluate the military utility of the Firebolt system in simulating representative threat targets for weapon system evaluation and training.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE