Studies on Ignition Over Pressure Characteristics Related to Typical Launch Vehicle Lift-off

Author:

Venkatraman R.,Sankaran Sathiyavageeswaran,Ramakrishna V. Venkata,Das Debopam,Sundararajan T.

Publisher

Springer Singapore

Reference5 articles.

1. Broadwell JE, Tsu CN (1967) Transient pressures caused by rocket start and shutdown in ducted launchers. J Spacecraft 4(10):1323–1328

2. Dougherty NS, Nesman TE, Guest SH (1982) Shuttle SRB ignition overpressure: model suppression test program and flight results. JANNAF 13th Plume Technology Meeting Houston, Texas, USA, CPIA Publication 357:217–243

3. Lai S, Laspesa FS (1982) Ignition overpressure measured on STS lift-off and correlation with subscale model tests. JANNAF 13th Plume Technology Meeting Houston, Texas, USA, CPIA Publication 357:207–216

4. Canabal F, Frendi A (2002) A computational study of the ignition over-pressure for launch vehicles. In: AIAA 2002-2541, 8th AIAA/CEAS aeroacoustic conference and exhibit, Brekenridge, Colorado, USA

5. Varnier J (2002) Blast wave at ignition of the rocket engines. ISMA 2002, Louvain (Belgique), TP 2002-175

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