Earth-to-orbit launch system alternativesA robust earth-to-orbit (ETO) transportation system, designed to facilitate the continuing human exploration of space, is discussed. The concept stresses larger lift capability and minimized on-orbit operations, of which the assembly and refueling operations are given priority. The modularity of the system is based on the required compatibility with the Space Shuttle vehicle, and it offers resiliency and reduced development costs. The support of lunar and Mars missions is interrelated with the mission logistics, the design of a transfer vehicle, the extent of reusability, and the required on-orbit operations. The transfer systems, the magnitude and frequency of propellant deliveries, and some human transportation requirements are considered with respect to vehicle concepts and flight rate strategies.
Document ID
19910025598
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Teixeira, Charles (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1990
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 90-3895Report Number: AIAA PAPER 90-3895