A concept is presented for a flyby mission of the planet. The mission was sized for the 2001 time period, has a crew of three, uses all propulsive maneuvers, and requires 442 days. Such a flyby mission results in significantly smaller vehicles than would a landing mission, but of course loses the value of the landing and the associated knowledge and prestige. Stay time in the planet vicinity is limited to the swingby trajectory but considerable time still exists for enroute science and research experiments. All propulsive braking was used in the concept due to unacceptable g-levels associated with aerobraking on this trajectory. LEO departure weight for the concept is approximately 594,000 pounds
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Of the several new initiatives being contemplated by NASA after the Space Station, a manned expediti...
A variety of mission scenarios are compared in this thesis to assess the strengths and weaknesses of...
A concept is presented for a three man crew to fly by the planet Mars. The ground rule for the study...
Trajectory and mission requirement data are presented for Earth Mars opposition and conjunction clas...
Mars flyby trajectories and Earth return trajectories have the potential to enable lower- cost and s...
Traveling to Mars with a human crew poses challenges exceeding those facing the Apollo astronauts in...
Mars nonstop round-trip trajectories using gravity supplemented by propulsion or aerodynamic force
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjun...
The purpose of this preliminary investigation is to analyze an end-to-end two-person Mars flyby miss...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
A discussion is presented of the basic principles of aerobraking. Typical results are given for the ...
AIAA Astrodynamics Specialist Conference August 2006, Keystone, CO.This paper explores trajectory o...
The concept of the Mars airplane was developed as a potential vehicle for unmanned Mars exploration....
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Of the several new initiatives being contemplated by NASA after the Space Station, a manned expediti...
A variety of mission scenarios are compared in this thesis to assess the strengths and weaknesses of...
A concept is presented for a three man crew to fly by the planet Mars. The ground rule for the study...
Trajectory and mission requirement data are presented for Earth Mars opposition and conjunction clas...
Mars flyby trajectories and Earth return trajectories have the potential to enable lower- cost and s...
Traveling to Mars with a human crew poses challenges exceeding those facing the Apollo astronauts in...
Mars nonstop round-trip trajectories using gravity supplemented by propulsion or aerodynamic force
A number of manned Mars mission types, propulsion systems, and operational techniques are compared. ...
This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjun...
The purpose of this preliminary investigation is to analyze an end-to-end two-person Mars flyby miss...
Earth-to-Mars distances vary from 60 to 400 million kilometers over a 14-year cycle. This complicate...
A discussion is presented of the basic principles of aerobraking. Typical results are given for the ...
AIAA Astrodynamics Specialist Conference August 2006, Keystone, CO.This paper explores trajectory o...
The concept of the Mars airplane was developed as a potential vehicle for unmanned Mars exploration....
The requirements, issues, and design options are reviewed for manned Mars landers. Issues such as hi...
Of the several new initiatives being contemplated by NASA after the Space Station, a manned expediti...
A variety of mission scenarios are compared in this thesis to assess the strengths and weaknesses of...