Title:
Shuttle Derived Launch Vehicles
a Solution for Space Access
Shuttle Derived Launch Vehicles
a Solution for Space Access
Author(s)
Furfaro, James A.
Johnson, Dennis G.
Johnson, Dennis G.
Advisor(s)
Editor(s)
Collections
Supplementary to
Permanent Link
Abstract
President George W. Bush set the bold vision and charter for NASA to
take the next steps in the exploration of our solar system in his
announcement on 14 January 2004. This exploration initiative provides
unique opportunities for the space community to work closely with
NASA to accomplish tasks that have been planned since the Apollo era.
In order for the NASA exploration initiative to be successful in today’s
environment, it must be reliable, affordable, and sustainable within a
realistic schedule.
Trade studies indicate that a two stage, solid / liquid configuration using
available heritage propulsion components is the most effective solution
to meet NASA’s schedule for crew access to space and the International
Space Station (ISS). Facilities and manpower are in place to process and
refurbish stage components maintaining a man-rated launch vehicle
infrastructure.
A heavy lift vehicle configuration can be tailored to support Moon and
Mars missions utilizing existing components. Lift capability can be
expanded with five segment RSRM derivative boosters and an extended
external tank. Shuttle derived launch vehicles provide the most reliable
and effective solution to meet NASA’s exploration vision schedule.
Sponsor
AIAA Space Systems Technical Committee ; AIAA Space Transportation Systems Technical Committee ; Space Technology Advanced Research Center
Date Issued
2005-11-10
Extent
212449 bytes
1905 bytes
212449 bytes
1905 bytes
212449 bytes
Resource Type
Text
Resource Subtype
Presentation