A 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 re...
A spin-tunnel investigation of the spin and recovery characteristics of a 1/25-scale model to the Ge...
The new RPAS (remotely piloted aerial systems) are mostly video cameras with wings whose ownership i...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/24-scale ...
A tail mounted spin recovery parachute system was designed and developed by the NASA Langley Researc...
A spin tunnel study is reported on a scale model of a research airplane typical of low-wing, single-...
A compilation of design considerations applicable to spin-recovery parachute systems for military ai...
An investigation was conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale model of ...
The present paper presents the results of a brief investigation made to determine the effectiveness ...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel on a l/18-scale mode...
An investigation was conducted in the Langley Spin Tunnel of the spin and spin-recovery characterist...
A supplementary investigation has been conducted in the Langley 20-foot free-spinning tunnel of a l/...
A spin-tunnel investigation of a 1/26 scale model of the Douglas XTB2D-1 airplane has been conducted...
An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect an...
The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery ...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
A spin-tunnel investigation of the spin and recovery characteristics of a 1/25-scale model to the Ge...
The new RPAS (remotely piloted aerial systems) are mostly video cameras with wings whose ownership i...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/24-scale ...
A tail mounted spin recovery parachute system was designed and developed by the NASA Langley Researc...
A spin tunnel study is reported on a scale model of a research airplane typical of low-wing, single-...
A compilation of design considerations applicable to spin-recovery parachute systems for military ai...
An investigation was conducted in the Langley 20-foot free-spinning tunnel on a 1/20-scale model of ...
The present paper presents the results of a brief investigation made to determine the effectiveness ...
An investigation has been conducted in the Langley 20-foot free-spinning tunnel on a l/18-scale mode...
An investigation was conducted in the Langley Spin Tunnel of the spin and spin-recovery characterist...
A supplementary investigation has been conducted in the Langley 20-foot free-spinning tunnel of a l/...
A spin-tunnel investigation of a 1/26 scale model of the Douglas XTB2D-1 airplane has been conducted...
An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect an...
The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery ...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
A spin-tunnel investigation of the spin and recovery characteristics of a 1/25-scale model to the Ge...
The new RPAS (remotely piloted aerial systems) are mostly video cameras with wings whose ownership i...
A spin investigation has been conducted in the Langley 20-foot free-spinning tunnel on a 1/24-scale ...