The three advanced propulsion systems analyzed are an advanced chemical system, an improved solid-core nuclear rocket engine with a 25-kilowatt auxiliary powerplant, and a nuclear-electric system. The comparison of these systems is made on the basis of transportation cost divided by the expected value of the data returned to earth. The analysis shows that for the Mercury Orbiter mission and for missions to the outer planets with a high data requirement, the nuclear-electric system emerges as the best system. For the Venus Orbiter mission, the advanced chemical propulsion system is best
A brief comparison is made between opposition class (with three impulse return), conjunction class, ...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) syst...
A detailed; mission-level systems study has been performed to show the benefit resulting from engine...
Cost and performance comparisons are made between chemical propulsion and nuclear electric propulsio...
honors thesisCollege of SciencePhysics and AstronomyClayton WilliamsThe Solar System has multiple d...
Space missions using electric propulsion systems launched by Saturn V or larger boosters - use of ch...
Trajectory profiles and nuclear propulsion vehicle configurations for manned Mars and Mars-Venus mis...
Equations and charts are presented that permit rapid estimation of propulsion-system performance req...
This report describes a study to evaluate the benefits of advanced propulsion technologies for trans...
Evaluation of 3-axis stabilized, 50-lb science payload spacecraft, Jupiter flyby and orbiter mission...
The possibility of implementing the solar probe project by launching a research satellite into the s...
This presentation describes a number of advanced space propulsion technologies with the potential fo...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
Missions with planned launch dates several years from today pose significant design challenges in pr...
Space mission requirements and technical feasibility of non-chemical space propulsion syste
A brief comparison is made between opposition class (with three impulse return), conjunction class, ...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) syst...
A detailed; mission-level systems study has been performed to show the benefit resulting from engine...
Cost and performance comparisons are made between chemical propulsion and nuclear electric propulsio...
honors thesisCollege of SciencePhysics and AstronomyClayton WilliamsThe Solar System has multiple d...
Space missions using electric propulsion systems launched by Saturn V or larger boosters - use of ch...
Trajectory profiles and nuclear propulsion vehicle configurations for manned Mars and Mars-Venus mis...
Equations and charts are presented that permit rapid estimation of propulsion-system performance req...
This report describes a study to evaluate the benefits of advanced propulsion technologies for trans...
Evaluation of 3-axis stabilized, 50-lb science payload spacecraft, Jupiter flyby and orbiter mission...
The possibility of implementing the solar probe project by launching a research satellite into the s...
This presentation describes a number of advanced space propulsion technologies with the potential fo...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
Missions with planned launch dates several years from today pose significant design challenges in pr...
Space mission requirements and technical feasibility of non-chemical space propulsion syste
A brief comparison is made between opposition class (with three impulse return), conjunction class, ...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) syst...
A detailed; mission-level systems study has been performed to show the benefit resulting from engine...