This paper introduces an evolvable Space Shuttle derived family of launch vehicles. It details the steps in the evolution of the vehicle family, noting how the evolving lift capability compares with the evolving lift requirements. A system description is given for each vehicle. The cost of each development stage is described. Also discussed are demonstration programs, the merits of the SSME vs. an expendable rocket engine (RS-68), and finally, the next steps needed to refine this concept
The objective was to design both a Personnel Launch System (PLS) and a family of Heavy Lift Launch V...
The Space Shuttle program is ending and elements of the Constellation Program are either being cance...
This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospac...
The use of well understood, legacy elements of the Space Shuttle system could yield a near-term, hig...
Shuttle derivatives have been under study by the National Aeronautics and Space Administration (NASA...
This paper describes future space transportation launch vehicles presently under study by the NASA a...
The Shuttle-C will usher in a new era of transportation capability for the United States. It will pr...
Shuttle-Derived Launch Vehicle (SDLV) concepts have been developed by a collaborative team comprisin...
Shuttle derivatives have been under study by the National Aeronautics and Space Administration (NASA...
United States current and planned space activities identify the need for increased payload capacity ...
Manned Mars missions (MMMs) will require payloads to low Earth orbit (LEO) much heavier and larger t...
Every study of exploration capabilities since the Apollo Program has recommended the renewal of a he...
Under construction today, the National Aeronautics and Space Administration's (NASA) Space Launch Sy...
A Heavy Lift Launch Vehicle (HLLV) designed to deliver 300,000 lb to a 540 n mi circular polar orbit...
NASA is developing an unprecedented heavy-lift capability to enable human exploration beyond low Ear...
The objective was to design both a Personnel Launch System (PLS) and a family of Heavy Lift Launch V...
The Space Shuttle program is ending and elements of the Constellation Program are either being cance...
This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospac...
The use of well understood, legacy elements of the Space Shuttle system could yield a near-term, hig...
Shuttle derivatives have been under study by the National Aeronautics and Space Administration (NASA...
This paper describes future space transportation launch vehicles presently under study by the NASA a...
The Shuttle-C will usher in a new era of transportation capability for the United States. It will pr...
Shuttle-Derived Launch Vehicle (SDLV) concepts have been developed by a collaborative team comprisin...
Shuttle derivatives have been under study by the National Aeronautics and Space Administration (NASA...
United States current and planned space activities identify the need for increased payload capacity ...
Manned Mars missions (MMMs) will require payloads to low Earth orbit (LEO) much heavier and larger t...
Every study of exploration capabilities since the Apollo Program has recommended the renewal of a he...
Under construction today, the National Aeronautics and Space Administration's (NASA) Space Launch Sy...
A Heavy Lift Launch Vehicle (HLLV) designed to deliver 300,000 lb to a 540 n mi circular polar orbit...
NASA is developing an unprecedented heavy-lift capability to enable human exploration beyond low Ear...
The objective was to design both a Personnel Launch System (PLS) and a family of Heavy Lift Launch V...
The Space Shuttle program is ending and elements of the Constellation Program are either being cance...
This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospac...