The design and testing of a two-stage parachute system to recover a space telescope weighing up to 2000 pounds is described. The system consists of a 15-ft dia ribbon parachute reefed to 50% for 10 seconds and a 73-ft dia paraform or cross second stage reefed to 10% for 10 seconds. The results of eight drop tests and one operational rocket launched flight and recovery are presented. A successful operational recovery of a 1600-lb NASA space telescope was conducted. The payload was launched by a second stage Minuteman rocket to an altitude of about 300 miles above sea level
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
The Orion Pad Abort Test 1 was conducted at the US Army White Sands Missile range in May 2010. The c...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...
This research has developed a viable drogue parachute release system sufficient for recovering level...
The effects were evaluated of 1980 technology on the weight of recovery systems capable of decelerat...
Spacecraft parachute recovery systems, especially those with a parachute cluster, require testing to...
Recovery and reuse of the Space Shuttle solid rocket boosters was baselined to support the primary g...
First steps have been taken to qualify a family of parafoil systems capable of increasing the surviv...
A tail mounted spin recovery parachute system was designed and developed by the NASA Langley Researc...
The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery ...
Parachute configuration, dummy and modified recorder capsules, and drop tests for parachute recovery...
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur
High altitude flight test of reefed 12.2-meter-diameter disk-gap-band parachute with deployment at 2...
Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...
Preliminary parametric studies were performed to establish size, weight and packaging arrangements f...
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
The Orion Pad Abort Test 1 was conducted at the US Army White Sands Missile range in May 2010. The c...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...
This research has developed a viable drogue parachute release system sufficient for recovering level...
The effects were evaluated of 1980 technology on the weight of recovery systems capable of decelerat...
Spacecraft parachute recovery systems, especially those with a parachute cluster, require testing to...
Recovery and reuse of the Space Shuttle solid rocket boosters was baselined to support the primary g...
First steps have been taken to qualify a family of parafoil systems capable of increasing the surviv...
A tail mounted spin recovery parachute system was designed and developed by the NASA Langley Researc...
The design, fabricate and testing of a rocket recovery system is presented in this report. Recovery ...
Parachute configuration, dummy and modified recorder capsules, and drop tests for parachute recovery...
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur
High altitude flight test of reefed 12.2-meter-diameter disk-gap-band parachute with deployment at 2...
Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...
Preliminary parametric studies were performed to establish size, weight and packaging arrangements f...
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
The Orion Pad Abort Test 1 was conducted at the US Army White Sands Missile range in May 2010. The c...
A baseline for a space shuttle configuration utilizing four parallel-burn 120-in. diameter SRMS is p...