Key X-33 Events in 1996
Click on the date to go to a related news release and any associated photos.
Please note that the following is only a partial listing of key events for the
second half of 1996.
Many thanks to Ann Gaudreaux, NASA Langley Research Center; Tony Jacob, NASA
Marshall Space Flight Center; and Jim Cast, NASA Headquarters, for supplying the
news releases and photographs found here.
1996
A full-scale segment of a graphite-composite wing designed for a reusable launch
vehicle (RLV) was successfully "tested to failure" at NASA's Langley Research
Center. This was the first structural test of a full-scale component designed and
fabricated to validate the use of graphite-composite primary structures for RLVs.
The purpose of the test was to determine the maximum load that the wing-box could
carry as well as to understand how it would fail.
Vice President Al Gore announced today at the Jet Propulsion Laboratory in Pasadena,
California, that Lockheed Martin had won the competition for the X-33 Phase II contract
over contenders McDonnell Douglas and Rockwell International.
NASA filed Notice of Intent 96-118 with the Federal Register of its intention
to prepare an environmental impact statement (EIS) and to conduct scoping meetings
for the development and testing of the X-33 vehicle. The EIS addressed environmental
issues associated with the fabrication, assembly, testing, and preparation of the
flight operations and landing sites associated with the X-33 flight vehicle.
NASA's Director of Space Transportation, Gary Payton, and the Vice President
for Lockheed Martin's Reusable Launch Vehicle Program, T. K. Mattingly, held an informal
meeting at 11 a.m. EST on Wednesday, November 13th, to discuss program status and
answer questions on the X-33,. which was undergoing its Preliminary Design Review
that week in California to formalize the engineering baseline of the X-33 vehicle
prior to moving on to the detailed design phase.
Announcement of the completion of the three-day Preliminary Design Review (PDR)
for the X-33 Ground Support System and Launch Facility. Individual PDRs already had
been conducted on the aerospike engine, the hydrogen tank, the structure, and most
subsystems.
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