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Jummie Garba Week 1: January 18 th , 2007

Jummie Garba Week 1: January 18 th , 2007. Propulsion Ares I/Ares V: From LEO to HEO. Transfer Vehicles. Ares I: Orbital Launch: 2014 Payload: 24,500 kg Ares V: Orbital Launch: 2020 Payload: 124,600 kg. At LEO. ∆V = 10000 m/s Gravity losses Turning flight path Aerodynamic drag

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Jummie Garba Week 1: January 18 th , 2007

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  1. Jummie GarbaWeek 1: January 18th, 2007 PropulsionAres I/Ares V: From LEO to HEO

  2. Transfer Vehicles • Ares I: • Orbital Launch: 2014 • Payload: 24,500 kg • Ares V: • Orbital Launch: 2020 • Payload: 124,600 kg

  3. At LEO • ∆V = 10000 m/s • Gravity losses • Turning flight path • Aerodynamic drag • Correct maneuvers • Rocket Equation • Inert mass (mIN) • Propellant mass (mp) • Final mass at HEO

  4. References • http://www.astronautix.com/lvs/aresi.htm • http://www.astronautix.com/lvs/aresv.htm

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