34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 1998
DOI: 10.2514/6.1998-3873
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Linear Aerospike SR-71 Experiment (LASRE) - Aerospace propulsion hazard mitigation systems

Abstract: Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to

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Cited by 5 publications
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“…3). 2 The limits remained about the same throughout the LASRE flight envelope, extending up to 50,000 ft. 3 Calculation of combustion conditions at equilibrium or for detonation showed that, even for low flammable concentrations of hydrogen and oxygen, temperatures and pressures high enough for structural damage could develop. A conservative ground rule stated that the oxygen and hydrogen concentrations must be maintained below 4 percent during the entire mission, because any combustion in the pod was deemed unacceptable.…”
Section: Flammability Limitsmentioning
confidence: 99%
“…3). 2 The limits remained about the same throughout the LASRE flight envelope, extending up to 50,000 ft. 3 Calculation of combustion conditions at equilibrium or for detonation showed that, even for low flammable concentrations of hydrogen and oxygen, temperatures and pressures high enough for structural damage could develop. A conservative ground rule stated that the oxygen and hydrogen concentrations must be maintained below 4 percent during the entire mission, because any combustion in the pod was deemed unacceptable.…”
Section: Flammability Limitsmentioning
confidence: 99%