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AAE450 Spring 2009 Week 4 Project Timeline [Solomon Westerman] [PM]
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AAE450 Spring 2009 Website Updates MDR Posted Folder for Mass/Volume/Power budgets –Managed by STRC/THM –Make sure to get component parameters to your GL by Wed. evening so this budget can be in presentation [Solomon Westerman] [PM]
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AAE450 Spring 2009 Today List major design characteristics –Hard/Soft landing (Trajectory) –Locomotion type –Spin stabilization (OTV and/or Lander) –TLI trajectory type –Payload to lunar surface Discuss arbitrary mass payload –Scalability –Work forward from launch vehicle
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AAE450 Spring 2009 Design (Week)X0 (2)X1 (3,4)X2 (4)X3 (4)X4 (4) Main PurposeInitial designRefined GLXP design Scalability analysis Effect of firm landing Effect of spin stabilization LandingSoft (<10g’s) Firm (<100g’s) TBD LocomotionRover TBD TLIHohmann (cryo) Spiral (EP) Stabilization3-axis Spin OTV or lander Mass to Lunar surface ~250 kg~ 150 kg?As large as X1 will allow ~ 150 kg?
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