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Rockwell X-30

The Rockwell X-30 was an advanced technology demonstrator project for the National Aero-Space Plane (NASP), part of a United States project to create a single-stage-to-orbit (SSTO) spacecraft and passenger spaceliner. Started in 1986, it was cancelled in the early 1990s before a prototype was completed, although much development work in advanced materials and aerospace design was accomplished. While a goal of a future NASP was a passenger liner capable of two-hour flights from Washington to Tokyo, the X-30 was planned for a crew of two and oriented towards testing.

Development
The NASP concept is thought to have been derived from the "Copper Canyon" project of the Defense Advanced Research Projects Agency (DARPA), from 1982 to 1985. In his 1986 State of the Union Address, President Ronald Reagan called for "a new Orient Express that could, by the end of the next decade, take off from Dulles Airport, accelerate up to 25 times the speed of sound, attaining low earth orbit or flying to Tokyo within two hours". In April 1986, McDonnell Douglas, Rockwell International, and General Dynamics were awarded contracts (each no more than $35 M) to develop technology for a hypersonic air-breathing SSTO vehicle/airframe. It is on display at the Aviation Challenge campus of the U.S. Space & Rocket Center in Huntsville, Alabama. ==Design==
Design
The original concept was for a conical nose, this evolved (after 1987?) to a flat shovel shape. The X-30 configuration integrated engine and fuselage. The shovel-shaped forward fuselage generated a shock wave to compress air before it entered the engine. The aft fuselage formed an integrated nozzle to expand the exhaust. The engine between was a scramjet. At the time, no scramjet engine was close to operational. The aerodynamic configuration was an example of a waverider. Most of the lift was generated by the fuselage by compression lift. The "wings" were small fins providing trim and control. This configuration was efficient for high-speed flight, but would have made takeoff, landing and slow-speed flight difficult. Temperatures on the airframe were expected to be over a large part of the surface, with maxima of more than on the leading edges and portions of the engine. This required the development of high temperature lightweight materials, including alloys of titanium and aluminum known as gamma and alpha titanium aluminide, advanced carbon/carbon composites, and titanium metal matrix composite (TMC) with silicon carbide fibers. Titanium matrix composites were used by McDonnell Douglas to create a representative fuselage section called "Task D". The Task D test article was four feet high by eight feet wide by eight feet long. A carbon/epoxy cryogenic hydrogen tank was integrated with the fuselage section and the whole assembly, including volatile and combustible hydrogen, was successfully tested with mechanical loads and a temperature of 820 °C (1,500 °F) in 1992, just before program cancellation. ==Specifications (X-30 as designed)==
Specifications (X-30 as designed)
==Design and materials legacy==
Source: Wikipedia ↗
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