The Jupiter Launch System - A Direct Derivative of the Space Transportation System (STS)

Paper number

IAC-08.A5.3.4

Author

Mr. Stephen Metschan, TeamVision Corporation, United States

Year

2008

Abstract

The Vision for Space Exploration (VSE) represents a watershed opportunity to expand the breadth and depth of human exploration and development for this and future generations.  By removing a thirty year restriction on manned exploration beyond Low Earth Orbit (LEO) the VSE authorization represents a significant milestone in the United States’ Space Exploration Policy.

Included in the VSE authorization is the directive that “the Administrator shall, to the fullest extent possible consistent with a successful development program, use the personnel, capabilities, assets, and infrastructure of the Space Shuttle program in developing the Crew Exploration Vehicle, Crew Launch Vehicle, and a heavy-lift launch vehicle.”

This paper will detail how the Jupiter Launch System (JLS) is our best Space Transportation System (STS) derivative configuration path when evaluated in terms of safety, implementation time, performance, development risk, STS workforce transition, STS infrastructure retention, and available budget.  We will compare and contrast these JLS advantages in both the near and long term within the context of NASA’s current VSE implementation plan as outlined in the Exploration System Archeicture Study (ESAS).

Abstract document

IAC-08.A5.3.4.pdf

Manuscript document

IAC-08.A5.3.4.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.