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Marshall
Space Flight Center 1997 Phase 2 Prediction of Launch Vehicle Ignition Overpressure and Liftoff Acoustic Environments Applied Research Associates, Inc. Littleton, CO |
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INNOVATION
Prediction software has been developed to specify acoustic pressure loading (ignition overpressure and launch acoustics) produced during liftoff on the external surfaces of launch vehicles from the propulsion system. The launch vehicle and launch pad models are developed by interaction with the user, which allows a large variety of configurations and trajectories. Overpressure mitigation through water injection can also be predicted. |
Launch Acoustics and Ignition Overpressure Prediction Code |
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ACCOMPLISHMENTS
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COMMERCIALIZATION
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GOVERNMENT/SCIENCE
APPLICATIONS
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| For more information about this firm, please send e-mail to company representative | Acoustics/Vibroacoustics
, Aerodynamics
Curator: SBIR Support 8/23/05 |