Rocket Launch Trajectory Simulations Mechanism
Rocket Launch Trajectory Simulations Mechanism
- New search for: Margasahayam, Ravi
- New search for: Caimi, Raoul E.
- New search for: Hauss, Sharon
- New search for: Voska, N.
- New search for: Margasahayam, Ravi
- New search for: Caimi, Raoul E.
- New search for: Hauss, Sharon
- New search for: Voska, N.
The design and development of a Trajectory Simulation Mechanism (TSM) for the Launch Systems Testbed (LST) is outlined. In addition to being one-of-a-kind facility in the world, TSM serves as a platform to study the interaction of rocket launch-induced environments and subsequent dynamic effects on the equipment and structures in the close vicinity of the launch pad. For the first time, researchers and academicians alike will be able to perform tests in a laboratory environment and assess the impact of vibroacoustic behavior of structures in a moving rocket scenario on ground equipment, launch vehicle, and its valuable payload or spacecraft.
Document information
Rocket Launch Trajectory Simulations Mechanism
International Congress on Sound and Vibration ; 2002 ; Orlando, FL, United States
2002-01-01
Preprint
No indication
English