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Project Minerva: A low-cost manned Mars mission based on indigenous propellant productionProject Minerva is a low-cost manned Mars mission designed to deliver a crew of four to the Martian surface, using only two sets of two launches. Key concepts which make this mission realizable are the use of near-term technologies and in-situ propellant production, following the senario originally proposed by R. Zubrin of Martin Marietta. The first set of launches delivers two unmanned payloads into low earth orbit (LEO): one consists of an Earth Return Vehicle (ERV), a propellant production plant, and a set of robotic vehicles, and the second consists of the upper stage/trans-Mars injection (TMI) booster. In LEO, the two payloads are joined and inserted into a Mars transfer orbit. The landing on Mars is performed with the aid of multiple aerobraking maneuvers. On the Martian surface, the propellant production plant uses a Sabatier/electrolysis-type process to combine six tons of hydrogen brought from earth with carbon dioxide from the Martian atmosphere to produce 100 tons of liquid oxygen and methane, which are later used as the propellants for the rover expeditions and the manned return journey of the ERV. Once the in-situ propellant production is completed, approximately two years after the first set of launches, the manned portion of the mission leaves earth. This set of two launches is similar to that of the unmanned vehicles; the two payloads are the Manned Transfer Vehicle (MTV) and the upper stage/TMI booster. The MTV contains the manned rover and the habitat which houses the astronauts enroute to Mars and on the Martian surface. During the 180-day trip to Mars, artificial gravity is created by tethering the MTV to the TMI booster and inducing rotation. Upon arrival the MTV performs aerobraking maneuvers to land near the fully-fueled ERV, which will be used by the crew a year and a half later to return to earth. The mission entails moderate travel times with relatively low-energy conjunction-class trajectories and allows ample time for scientific exploration. This set of missions can be repeated every two years in order to continue exploration at a variety of sites and gradually establish the infrastructure for a permanent base on Mars.
Document ID
19940021212
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bruckner, Adam P.
(Washington Univ. Seattle, WA, United States)
Anderson, Hobie
(Washington Univ. Seattle, WA, United States)
Caviezel, Kelly
(Washington Univ. Seattle, WA, United States)
Daggert, Todd
(Washington Univ. Seattle, WA, United States)
Folkers, Mike
(Washington Univ. Seattle, WA, United States)
Fornia, Mark
(Washington Univ. Seattle, WA, United States)
Hamling, Steven
(Washington Univ. Seattle, WA, United States)
Johnson, Bryan
(Washington Univ. Seattle, WA, United States)
Kalberer, Martin
(Washington Univ. Seattle, WA, United States)
Machula, Mike
(Washington Univ. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: USRA, Proceedings of the 8th Annual Summer Conference: NASA(USRA Advanced Design Program
Subject Category
Propellants And Fuels
Accession Number
94N25705
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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