Launch failures - PowerPoint PPT Presentation

Launch Vehicle Failure Mode Database AST Research and Development Project

Federal Aviation Administration. Launch Vehicle Failure Mode Database AST Research and Development Project. Presented to: COMSTAC RLV Working Group By: Nickolas Demidovich Date: May 17, 2007. Overview. Historical Database Tasking Phase 1 Phase 2 Status Findings to date Overall

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AAE 450- Propulsion LV

AAE 450- Propulsion LV. Stephen Hanna Critical Design Review 02/27/01. 15.24m Max. 30.48 m. 24.00 m  NTR. {~8 m}. 54.864 m. 3.9 m. 7.985 m D. Launch Vehicle (Stephen Hanna). Energia Total Payload to LEO ~179 Tonnes $1.2 billion – $2.8 billion per launch (2000 dollars)

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241 views • 12 slides

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