A series of launch vehicles was proposed, based around the proposed Space Transportation Main Engine (STME) liquid-fuel rocket engine. The STME was to be a simplified, expendable version of the Space Shuttle main engine (SSME).[3][4] The NLS-1 was the largest of three proposed vehicles and would have used a modified Space Shuttle external tank for its core stage. The tank would have fed liquid oxygen and liquid hydrogen to four STMEs attached to the bottom of the tank. A payload or second stage would have fit atop the core stage, and two detachable Space Shuttle Solid Rocket Boosters would have been mounted on the sides of the core stage as on the Shuttle.[3] Period illustrations suggest that much larger rockets than NLS-1 were contemplated, using multiples of the NLS-1 core stage.[5][6]
Program cancellation
The NLS program did not venture beyond the planning stages and did not survive the Presidency of Bill Clinton, which started in January 1993. In 1992, Daniel Goldin was selected to replace Vice Admiral Richard H. Truly as NASA administrator. Goldin championed the motto,
"faster, better, cheaper,"[7] which may not have fit the ambitious NLS vision. A NASA history from 1998 says that reusable single-stage-to-orbit (SSTO) rockets and space planes such as the McDonnell Douglas DC-X and the Lockheed Martin X-33 seemed attainable and represented smaller, simpler alternatives to the sprawling Shuttle program.[8] The NLS, by contrast, was more of a continuation of the Shuttle legacy. By the beginning of the Clinton administration, the expensive Space Shuttle and planned Space Station Freedom programs had enough momentum to continue, and the SSTO projects showed enough promise to fund. There was no money left for another big program such as the NLS.[citation needed]
NASA later developed a very similar launch vehicle to NLS-1 called the Space Launch System, as part of its Artemis program to return astronauts to the Moon in the mid-2020s. The similarities include a lengthened Shuttle external tank-like core stage, four engines meant as expendable versions of the SSME, and large solid rocket boosters (with five segments instead of four).[11][12][13][14][15]
NASA History Division (September 23, 1998), "The Policy Origins of the X-33 Part II: The NASA Access to Space Study", X-33 History Project, National Aeronautics and Space Administration, archived from the original on October 22, 2014, retrieved April 25, 2010
Wood, B. K. (2002), "Propulsion for the 21st Century—RS-68", 38th Joint Liquid Propulsion Conference, Indianapolis, Indiana. July 2002. Reston, Virginia, USA., American Institute of Aeronautics and Astronautics, archived from the original on March 19, 2009, retrieved April 25, 2010
External links
EELV - Boeing Contains good summary of NLS from an early 1990s perspective.