The X-33 Program Takes Its Shape
by Andrzej Rucinski
The NASA X-33 Program, established in 1997, is designed to demonstrate the
key design and operational aspects of a Single Stage to Orbit (SSTO) Reusable
Launch Vehicle (RLV) rocket system. This approach is different from traditional
launchers that by definition are disposable and thus expensive. It is also
different from the space shuttle. The space shuttle is partially reusable, but
the operation and maintenance costs are enormous. The RLV goal is to lower the
cost from $10,000 per pound of payload to low earth orbit to $1,000 per pound.
Another distinguishable characteristic of the RLV program is to operate using
private venture capital and not federal funding. In order to encourage the
private sector in developing such a commercially viable system, the program is
conducted in two stages. The first one is the X-33 program that will lead to the
development of an experimental, reduced scale vehicle used as a technology
demonstrator. The second stage should result in a commercial space vehicle,
called the Venture Star. More information pertinent to this project can be found
at http://stp.msfc.nasa.gov/stpweb/x33/.
Currently, the X-33 is being assembled at Lockheed Martin Skunk Works in
Palmdale, California. The space plane will be powered with a new type of
aerospike engines that use liquid hydrogen and liquid oxygen. Two of the tanks
should be available shortly at Edwards Air Force Base, California. The base has
been designated as a testing center for X-33 with flights scheduled for early
2000. A total of 15 flights is planned. A major goal of these flights is the
demonstration of the system’s capability to handle the heat during a full-scale
RLV return from orbit.
UNH has been involved in the X-33 program for several years. The development
effort was conducted by a multidisciplinary team of students, both undergraduate
and graduates, through a grant sponsored by Sanders, a Lockheed Martin Company
(see "ECE Department Goes Beyond High Tech," Signals & Noise, Summer
1997). The purpose of the project was to design an advanced concept Remote
Health Node (RHN). Fifty RHNs are used on the X-33 to gather information about
its parameters such as temperature, stress, etc. One of the challenges was to
develop a reversible heat transfer mechanism to cool off the remote health node.
This challenge has required very close cooperation among mechanical and
electrical engineering students.