An introduction to the MAPSEP organization and a detailed analytical description of all models and algorithms are given. These include trajectory and error covariance propagation methods, orbit determination processes, thrust modeling, and trajectory correction (guidance) schemes. Earth orbital MAPSEP contains the capability of analyzing almost any currently projected low thrust mission from low earth orbit to super synchronous altitudes. Furthermore, MAPSEP is sufficiently flexible to incorporate extended dynamic models, alternate mission strategies, and almost any other system requirement imposed by the user. As in the interplanetary version, earth orbital MAPSEP represents a trade-off between precision modeling and computational speed co...
The detailed mission and system optimization of low thrust electric propulsion missions is a complex...
Computer program for determining performance and system requirements of electrically propelled space...
Nuclear-electric power generation system requirements for orbiter and flyby missions using Saturn V ...
The mission analysis program for solar electric propulsion (MAPSEP) is comprised of the basic modes:...
A revised user's manual for the computer program MAPSEP is presented. Major changes from the interpl...
A user's manual which describes input/output routines and recommended operating procedures relating ...
The internal structure of MAPSEP is described. Topics discussed include: macrologic, variable defini...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
Selected missions using solar electric propulsion and conventional propulsion systems were studied. ...
Computer program has been designed to handle computations for low thrust missions rapidly and with a...
A performance-analysis computer program, that was developed explicitly to generate optimum electric ...
Computer programs for solving trajectory and system optimization problems of electrically propelled ...
A summary is given of a one-year study to determine the applicability of solar electric propulsion a...
Solar electric propulsion characteristics and capability for automated missions throughout solar sys...
The development of an analysis which addresses the problems of degrading space environmental effects...
The detailed mission and system optimization of low thrust electric propulsion missions is a complex...
Computer program for determining performance and system requirements of electrically propelled space...
Nuclear-electric power generation system requirements for orbiter and flyby missions using Saturn V ...
The mission analysis program for solar electric propulsion (MAPSEP) is comprised of the basic modes:...
A revised user's manual for the computer program MAPSEP is presented. Major changes from the interpl...
A user's manual which describes input/output routines and recommended operating procedures relating ...
The internal structure of MAPSEP is described. Topics discussed include: macrologic, variable defini...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
Selected missions using solar electric propulsion and conventional propulsion systems were studied. ...
Computer program has been designed to handle computations for low thrust missions rapidly and with a...
A performance-analysis computer program, that was developed explicitly to generate optimum electric ...
Computer programs for solving trajectory and system optimization problems of electrically propelled ...
A summary is given of a one-year study to determine the applicability of solar electric propulsion a...
Solar electric propulsion characteristics and capability for automated missions throughout solar sys...
The development of an analysis which addresses the problems of degrading space environmental effects...
The detailed mission and system optimization of low thrust electric propulsion missions is a complex...
Computer program for determining performance and system requirements of electrically propelled space...
Nuclear-electric power generation system requirements for orbiter and flyby missions using Saturn V ...