
University of Tennessee SSTA - Google Sites
SSTA is built on a collective vision to push boundaries. All UT students interested are encouraged to apply for membership in our Fall or Spring cycles here.
- University of Tennessee
Our members are diverse and talented, with students from all backgrounds and representing most STEM fields. Prospective members are encouraged to attend our weekly meetings on …
University of Tennessee SSTA - Projects - Google Sites
UTK's first self-pressurizing bipropellant liquid rocket engine! More Information. A 1,200 lb. thrust hybrid rocket that flew to 28,878 ft and reached Mach 1.77 at Spaceport America in...
University of Tennessee SSTA - Big Hybrid
The Highest Thrust, Highest Impulse, Highest Efficiency Rocket Motor Ever Tested at UTK. 1,850 lbs - peak thrust. 1,200 lbs - average thrust. 7,250 lbf-s - impulse (half O-motor). Credited by …
Student Space Technology Association | LinkedIn
The Student Space Technology Association (SSTA) at the University of Tennessee, Knoxville is on a mission to pursue complex aerospace engineering problems, with an ambitious goal of …
Student Space Technology Association @ UTK · GitHub
We are a student group at the University of Tennessee, Knoxville dedicated to the design, construction, and flight of rockets. Open-Source filament winding program with the primary …
University of Tennessee SSTA - Join
Apply to Join SSTA! - Attend our meetings! Our shop is located behind the Allen Jones Aquatic Center, in the Fleet Services Parking lot. At the beginning of each semester, we host an …
SSTA-UTK/SSTA-UTK: SSTA wiki - GitHub
SSTA wiki. Contribute to SSTA-UTK/SSTA-UTK development by creating an account on GitHub.
UTK Student Space Technology Association - SECO SEALS, Inc.
2025年3月11日 · SSTA focuses on hybrid and liquid rocket propulsion projects in addition to high-altitude balloons and high-power rocketry certifications. Notably, SSTA won 1st place in the …
University of Tennessee SSTA - Teams - Google Sites
Fluid Control Systems - Develop and test innovative valve mechanisms for precise control of propellant flow in SSTA’s rocket engines. Thrust Vector Control - Engineer and integrate …
- 某些结果已被删除