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... the Journal of the British Interplanetary Society for Volume 59 59
'''Page ''' - 230-238
'''Year''' - 2006
'''Keywords''' - Human exploration missions, electric propulsion, lunar mission architectures, space architectures, Mars mission architectures, space exploration cost, cost reduction
'''JBIS Reference Code ''' - 2006.59.230
'''Number of Pages''' - 9
Abstract
The cost of human exploration missions has been and ...
... are presented for large, high-power nuclear and solar electric spacecraft, based on a trade-off analysis of power/ propulsion technology options and an optimisation of the complete mission design to the minimise the total response time for a representative impactor/deflection scenario. High ...
... design study was performed for the NASA Radioisotope Power Systems Office to explore the use of radioisotope electric propulsion for flagship class missions. The Kuiper Belt Object Orbiter is a flagship class mission concept projected for launch in the 2030 timeframe. Due to the large size of a flagship class science mission larger radioisotope power ...
... propulsive maneuver, solar sails, and large fission-reactor-powered nuclear electric propulsion systems. We present an alternative approach - the Innovative Interstellar Explorer - based on Radioisotope Electric Propulsion. A high ... mission and spacecraft design. We also discuss the role such a mission plays in assessing heliospheric "space climate," knowledge of which is vital for human exploration ...
... exploration would take advantage of developments in equipment miniaturization and new technologies, using a sharply focussed mission objective to reduce spacecraft size and mission costs. An example micromission to Ceres using solar-electric propulsion ...
... mission goal was to demonstrate Solar Electric Primary Propulsion by orbit raising from Geostationary Transfer Orbit to the Moon. Due to favourable thruster and power ...
... electric propulsion, recovery strategies
'''JBIS Reference Code ''' - 2009.62.362
'''Number of Pages''' - 7
Abstract
ESA's BepiColombo is the first mission to fly to Mercury by using solar electric propulsion as primary propulsion ...
...
'''Year''' - 2006
'''Keywords''' - Electric propulsion, hollow cathode, colloid, thruster, PPT
'''JBIS Reference Code ''' - 2006.59.176
'''Number of Pages''' - 8
Abstract
The use of electric propulsion for near Earth and deep space missions has occurred due to long term research into understanding the physical phenomena occurring within various propulsion subsystems. This research has resulted ...
... for lunar industries, not building and operating the lunar infrastructure. NASA should not be responsible for producing the lunar oxygen for missions, building the solar power arrays required for ... for development of lunar resources and conducting the preliminary human exploration ...
... for Volume 60 60
'''Page ''' - 63-71
'''Year''' - 2007
'''Keywords''' - Small spacecraft, electric propulsion, electric propulsion missions, electric thrusters, solar cells, solar ... power production, from much improved solar cells and solar arrays. This has allowed electric propulsion (EP) systems to become viable for ...
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