AAE450 Senior Spacecraft Design Nathan Payne March 29 th, 2007 Final Presentation.

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Presentation transcript:

AAE450 Senior Spacecraft Design Nathan Payne March 29 th, 2007 Final Presentation

AAE450 Senior Spacecraft Design Payne - 2 Transfer Vehicle Communication Dishes Specifications CAD’s provided by Matt Fox Constant coverage for duration of all missions Enough propellant to execute mid- course burns both to and from Mars Two dishes on TV for redundancy Docking for departure and arrival burns

AAE450 Senior Spacecraft Design Payne - 3 Transfer Vehicle Artificial Gravity Propellant Needs Artificial gravity spin-up propellant contained within the TV Engine nozzles for spin-up on TV All other propellant in large tanks at opposite end of the truss from the TV Spin-up maneuver takes less than 30min TV is spun-up after the Earth and Mars departure burns TV is spun-down after the Earth and Mars arrival burns Artificial gravity still active during mid-course burns CAD provided by Matt Fox

AAE450 Senior Spacecraft Design Payne - 4 Backup Slides

AAE450 Senior Spacecraft Design Payne Mission Scenarios 1 st 2 nd 3 rd 4 th HEO -dE HMO-aM HMO-dM HEO-aE

AAE450 Senior Spacecraft Design Payne - 6 References Hall, Theodore W., “Artificial Gravity and the Architecture of Orbital Habits,” 1997, sec. 3-6, ecture_of_orbital_habitats.shtml, [retrieved Jan 2007] ecture_of_orbital_habitats.shtml “NASA’s Exploration Systems Architecture Study,” NASA-TM , November 2005, sec.5, pp , t.html, [retrieved Jan 2007] t.html Landau, Dr. Damon F., “Strategies for the Sustained Human Exploration of Mars,” West Lafayette, IN, Dec. 2006, Chp. 9, pp Longuski, James M., “Galileo Maneuver Analysis,” Lake Tahoe, NV, August 1981, pp. 3-4 Code from week 8 presentation