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AAE 450- Propulsion LV Stephen Hanna Design Review 02/19/01.

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Presentation on theme: "AAE 450- Propulsion LV Stephen Hanna Design Review 02/19/01."— Presentation transcript:

1 AAE 450- Propulsion LV Stephen Hanna Design Review 02/19/01

2 Launch Vehicle (Stephen Hanna)
Energia Total Payload to LEO ~179 Tonnes Mass 3rd Stage payload (HAB & ERV) ~75 Tonnes Mass 3rd Stage Propulsion system ~75 Tonnes $1.2 billion – $2.8 billion per launch (2000 dollars) All facilities Exist Available for licensed production overseas 50 ft = 15.24………100 ft = m ……… 12.8 f t= 3.9 m ……… 26.2 ft = m 131 ft = m ……… 180 ft = m 50 ft = Picture from NASA DRM 100 ft = 30.48 180 ft = m

3 Abort Scenario (Stephen Hanna)
Ejection Seats Self Contained Pyrotechnics for escape ~1 tonne (204kg each*4 crew = 816 kg total) Proven at varied speeds and altitudes Picture from


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