NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A spin-recovery parachute system for light general-aviation airplanesA tail mounted spin recovery parachute system was designed and developed for use on light general aviation airplanes. The system was designed for use on typical airplane configurations, including low wing, high wing, single engine and twin engine designs. A mechanically triggered pyrotechnic slug gun is used to forcibly deploy a pilot parachute which extracts a bag that deploys a ring slot spin recovery parachute. The total system weighs 8.2 kg. System design factors included airplane wake effects on parachute deployment, prevention of premature parachute deployment, positive parachute jettison, compact size, low weight, system reliability, and pilot and ground crew safety. Extensive ground tests were conducted to qualify the system. The recovery parachute was used successfully in flight 17 times.
Document ID
19800015021
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bradshaw, C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: Proc. of the 14th Aerospace Mech. Symp.
Subject Category
Aircraft Stability And Control
Accession Number
80N23512
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available