This report describes a study to evaluate the benefits of advanced propulsion technologies for transporting materials between low Earth orbit and the Moon. A relatively conventional reference transportation system, and several other systems, each of which includes one advanced technology component, are compared in terms of how well they perform a chosen mission objective. The evaluation method is based on a pairwise life-cycle cost comparison of each of the advanced systems with the reference system. Somewhat novel and economically important features of the procedure are the inclusion not only of mass payback ratios based on Earth launch costs, but also of repair and capital acquisition costs, and of adjustments in the latter to reflect the...
37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit Salt Lake City, UT, July 8-11, 2001...
The paper presents and discuses a concept for a Moon mission which enables to prove and validate sev...
Space transportation requirements for the NASA baseline scenario for future space missions are discu...
We report on a study to evaluate tie benefits of advanced Imgptd, qon technologies for transpom&apos...
This brief work discusses a possible application of a tether as a dynamical element in a low Earth o...
Using electric propulsion to deliver materials to lunar orbit for the development and construction o...
The feasibility of returning humans to the Moon by 2004, the 35th anniversary of the Apollo 11 landi...
Lunar transportation architectures exist for several different mission scenarios. Direct flights fro...
A amplified computational model of low Earth or_t-Moon transportation systems has been d_eloped to p...
The question of using lunar produced propellants in a logistic operation of a lunar base has been st...
Important to the planning for a lunar base is the development of transportation requirements for the...
Summary The paper proposes a concept mission to Moon including a space-tug-vehicle in Moon orbit,...
In this paper, optimum trajectories in Earth Transfer Orbit (ETO) for a lunar transportation system ...
It is well known that propellants produced at the points of destination such as the Moon or Mars wil...
AURORA is ESA’ long term technology program devoted to prepare human exploration missions within the...
37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit Salt Lake City, UT, July 8-11, 2001...
The paper presents and discuses a concept for a Moon mission which enables to prove and validate sev...
Space transportation requirements for the NASA baseline scenario for future space missions are discu...
We report on a study to evaluate tie benefits of advanced Imgptd, qon technologies for transpom&apos...
This brief work discusses a possible application of a tether as a dynamical element in a low Earth o...
Using electric propulsion to deliver materials to lunar orbit for the development and construction o...
The feasibility of returning humans to the Moon by 2004, the 35th anniversary of the Apollo 11 landi...
Lunar transportation architectures exist for several different mission scenarios. Direct flights fro...
A amplified computational model of low Earth or_t-Moon transportation systems has been d_eloped to p...
The question of using lunar produced propellants in a logistic operation of a lunar base has been st...
Important to the planning for a lunar base is the development of transportation requirements for the...
Summary The paper proposes a concept mission to Moon including a space-tug-vehicle in Moon orbit,...
In this paper, optimum trajectories in Earth Transfer Orbit (ETO) for a lunar transportation system ...
It is well known that propellants produced at the points of destination such as the Moon or Mars wil...
AURORA is ESA’ long term technology program devoted to prepare human exploration missions within the...
37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit Salt Lake City, UT, July 8-11, 2001...
The paper presents and discuses a concept for a Moon mission which enables to prove and validate sev...
Space transportation requirements for the NASA baseline scenario for future space missions are discu...