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Project ExodusA design for a manned Mars mission, PROJECT EXODUS is presented. PROJECT EXODUS incorporates the design of a hypersonic waverider, cargo ship and NIMF (nuclear rocket using indigenous Martian fuel) shuttle lander to safely carry out a three to five month mission on the surface of Mars. The cargo ship transports return fuel, return engine, surface life support, NIMF shuttle, and the Mars base to low Mars orbit (LMO). The cargo ship is powered by a nuclear electric propulsion (NEP) system which allows the cargo ship to execute a spiral trajectory to Mars. The waverider transports ten astronauts to Mars and back. It is launched from the Space Station with propulsion provided by a chemical engine and a delta velocity of 9 km/sec. The waverider performs an aero-gravity assist maneuver through the atmosphere of Venus to obtain a deflection angle and increase in delta velocity. Once the waverider and cargo ship have docked the astronauts will detach the landing cargo capsules and nuclear electric power plant and remotely pilot them to the surface. They will then descend to the surface aboard the NIMF shuttle. A dome base will be quickly constructed on the surface and the astronauts will conduct an exploratory mission for three to five months. They will return to Earth and dock with the Space Station using the waverider.
Document ID
19900016710
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bryant, Rodney
(Maryland Univ. College Park, MD, United States)
Dillon, Jennifer
(Maryland Univ. College Park, MD, United States)
Grewe, George
(Maryland Univ. College Park, MD, United States)
Mcmorrow, Jim
(Maryland Univ. College Park, MD, United States)
Melton, Craig
(Maryland Univ. College Park, MD, United States)
Rainey, Gerald
(Maryland Univ. College Park, MD, United States)
Rinko, John
(Maryland Univ. College Park, MD, United States)
Singh, David
(Maryland Univ. College Park, MD, United States)
Yen, Tzu-Liang
(Maryland Univ. College Park, MD, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Subject Category
Astronautics (General)
Report/Patent Number
ENAE-412
NAS 1.26:186836
NASA-CR-186836
UM-AERO-90-28
Accession Number
90N26026
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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