Publication Date:
2019-07-13
Description:
As part of comprehensive efforts to develop physics-based risk assessment techniques for space systems at NASA, coupled computational fluid and rigid body dynamic simulations were carried out to investigate the flow mechanisms that accelerate tank fragments in bursting pressurized vessels. Simulations of several configurations were compared to analyses based on the industry-standard Baker explosion model, and were used to formulate an improved version of the model. The standard model, which neglects an external fluid, was found to agree best with simulation results only in configurations where the internal-to-external pressure ratio is very high and fragment curvature is small. The improved model introduces terms that accommodate an external fluid and better account for variations based on circumferential fragment count. Physics-based analysis was critical in increasing the model's range of applicability. The improved tank burst model can be used to produce more accurate risk assessments of space vehicle failure modes that involve high-speed debris, such as exploding propellant tanks and bursting rocket engines.
Keywords:
Aerodynamics; Launch Vehicles and Launch Operations
Type:
ARC-E-DAA-TN14375
,
Probablistic Safety Assessment and Management Conference (PSAM 12); Jun 22, 2014 - Jun 27, 2014; Honolulu, HI; United States
Format:
application/pdf
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