Graham2001
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A long time ago Kev Shanow made a [ame=http://www.orbithangar.com/searchid.php?ID=670]hot air balloon for orbiter[/ame], which is quite fun, but has never been updated since Orbiter 2003.
More recently I found several documents relating to NASA's tests of various re-entry parachutes for what became the Viking program. They suspended a model entry vehicle from a balloon and then released the vehicle at an altitude of 40,000m to allow the parachute to be tested. This might prove to be an interesting add-on for Orbiter.
See:
1. Flight test of a 15-foot-diameter (4.6-meter) 120 deg conical spacecraft simulating parachute deployment in a Mars atmosphere
2. Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment (Film)
3. Performance of a 16.6-meter-diameter modified ringsail parachute in a simulated Martian environment (Film)
4. Performance of a 19.7 meter diameter disk gap band parachute in a simulated Martian environment (Film)
5. Inflation and performance of three parachute configurations from supersonic flight tests in a low-density environment
Note: There were a number of sounding rocket based tests in the same series which I am currently trying to run down.
More recently I found several documents relating to NASA's tests of various re-entry parachutes for what became the Viking program. They suspended a model entry vehicle from a balloon and then released the vehicle at an altitude of 40,000m to allow the parachute to be tested. This might prove to be an interesting add-on for Orbiter.
See:
1. Flight test of a 15-foot-diameter (4.6-meter) 120 deg conical spacecraft simulating parachute deployment in a Mars atmosphere
2. Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment (Film)
3. Performance of a 16.6-meter-diameter modified ringsail parachute in a simulated Martian environment (Film)
4. Performance of a 19.7 meter diameter disk gap band parachute in a simulated Martian environment (Film)
5. Inflation and performance of three parachute configurations from supersonic flight tests in a low-density environment
Note: There were a number of sounding rocket based tests in the same series which I am currently trying to run down.
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