NASA/SP-8030, Transient Loads From Thrust Excitation, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), February,1969, pp. 28, Format(s): PDF 1320k |
Analysis of transient loads produced by ignition of rocket engine during launch and flight operations for solid and liquid propellant rocket engines
| Keywords: | liquid propellant rocket engines, solid propellant rocket engines, transient loads, transient response, combustion physics, ignition, rocket flight, rocket launching |
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| CASI Document ID Number: | 71N24281 |
| Subjects: | Engineering: Structural Mechanics: Stresses and Loads |
| ID Code: | 23 |
| Deposited On: | 13 May 2002 |