David Wolf was born on August 23, 1956, in Indianapolis, Indiana. Wolf graduated with distinction from Purdue University with a degree in electrical engineering. He then earned a medical degree from Indiana University School of Medicine, and trained as a flight surgeon with the United States Air Force. In 1983, Wolf worked at the Johnson Space Center to study the physiological effects of microgravity. Wolf was then assigned as chief engineer for the design of the medical facility of the Space Station. In 1990, Wolf was selected as an astronaut candidate. After training, Wolf was selected as an astronaut, and would go on four space flights–the STS-59, Mir Expedition 24, STS-112, and STS-127. He had a total of 7 EVAs, and spent 168 days in space. After the missions, Wolf worked as the Managing Director for EarthTomorrow, Inc., and was a visiting professor at Purdue University. Currently, he is the Chief Technology Officer for Voxel Systems.
Quick Facts
Diameter |
5 in |
|---|---|
Length |
102 in |
Designed Launch Weight |
54.3 lbm |
Predicted Simulation Apogee |
4968 ft |
Achieved Apogee |
5191 ft |
Motor |
Loki L930 |
Average Thrust |
209 lbf |
Payload |
Real-time sensor data transmission |
Results
This year, the payload challenge was to have the STEMnaut ‘crew’ relay real-time data to mission control. It consisted of four subsystems: the STEMnaut capsule, the radio transmission system, the sensor package, and the parachute release latch. Payload was successful during the competition launch, as 18 transmissions were received. Construction and Avionics components were also successful during the launch, as altimeters and parachutes were deployed correctly, and the launch vehicle operated as expected. Additionally, improvements made on the Flight Recording System led to a successful recorded flight video during the competition launch.
The Student Launch team placed 9th in the overall competition, as well as 3rd in the Safety Award.
Additional Specs
Launch Rail Size |
144″ 1515 |
|---|---|
Recovery System |
Dual Deployment at Apogee and 700 ft AGL |
Booster and RnD Coupler Mass |
6.93 lbm |
Avionics and Recovery Mass |
11.83 lbm |
Payload Mass |
10.64 lbm |
Motor |
Loki L930 |
Ballast Flown |
1 lbm |
TWR |
5.6 |