Rockwell X-30

Last updated

X-30 NASP
X-30 NASP 3.jpg
An artist's concept of the X-30 entering orbit
General information
Type Single-stage-to-orbit (SSTO) spaceplane
Manufacturer Rockwell International
StatusCancelled in 1993
Primary user NASA

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. [1] 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 completed. While a goal of a future NASP was a passenger liner (the Orient Express) capable of two-hour flights from Washington to Tokyo, [1] the X-30 was planned for a crew of two and oriented towards testing.[ citation needed ]

Contents

An older design model on display at the U.S. Space & Rocket Center in Huntsville, Alabama; note the conical nose and single-dorsal fin tail that distinguishes it from the newer model. Rockwell X-30 Older Design.png.jpg
An older design model on display at the U.S. Space & Rocket Center in Huntsville, Alabama; note the conical nose and single-dorsal fin tail that distinguishes it from the newer model.
A newer design mockup on display at the Aviation Challenge campus of the U.S. Space & Rocket Center in Huntsville, Alabama; note the flat, duckbill nose and double-dorsal fin tail that distinguishes it from the older model. Rockwell X-30 Newer Design.png.jpg
A newer design mockup on display at the Aviation Challenge campus of the U.S. Space & Rocket Center in Huntsville, Alabama; note the flat, duckbill nose and double-dorsal fin tail that distinguishes it from the older model.

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". [1]

Research suggested a maximum speed of Mach 8 for scramjet-based aircraft, as the vehicle would generate heat due to adiabatic compression, which would expend considerable energy. The project showed that much of this energy could be recovered by passing hydrogen over the skin and carrying the heat into the combustion chamber: Mach 20 then seemed possible. The result was a program funded by NASA, and the United States Department of Defense (funding was approximately equally divided among NASA, DARPA, the US Air Force, the Strategic Defense Initiative Office (SDIO) and the US Navy). [2]

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. [2] Rocketdyne and Pratt & Whitney were each awarded contracts of $175 M to develop engines/propulsion. [2] The airframe contractors would compete and two or three would be eliminated after a year. [2] The plan was that 42 months later (end of 1989), contracts would be awarded to build the flight demonstrator vehicle. [2]

In 1990, the companies joined under the direction of Rockwell International to develop the craft, to deal with the technical and budgetary obstacles.[ citation needed ] Development of the X-30, as it was then designated, began.[ citation needed ]

Despite progress in the necessary structural and propulsion technology, NASA had substantial problems to solve.[ citation needed ] The Department of Defense wanted it to carry a crew of two and a small payload. The demands of being a human-rated vehicle, with instrumentation, environmental control systems and safety equipment, made the X-30 larger, heavier, and more expensive than required for a technology demonstrator. The X-30 program was terminated amid budget cuts and technical concerns in 1993.[ citation needed ]

Legacy

A more modest hypersonic program culminated in the uncrewed X-43 "Hyper-X".[ citation needed ]

A detailed, one-third scale (50-foot long) mockup of the X-30 was built by engineering students at Mississippi State University's Raspet Flight Research Laboratory in Starkville, Mississippi. [3] [4] [5] It is on display at the Aviation Challenge campus of the U.S. Space & Rocket Center in Huntsville, Alabama. [6]

Design

A 1986 artist's concept of the NASP on liftoff X-30 futuristic nasa.jpg
A 1986 artist's concept of the NASP on liftoff
An artist's concept of the X-30 in orbit X-30 NASP 1.jpg
An artist's concept of the X-30 in orbit
An artist's concept of the X-30 on re-entry X-30 NASP 2.jpg
An artist's concept of the X-30 on re-entry
An X-30 model in a wind tunnel X-30 NASP 4.jpg
An X-30 model in a wind tunnel

The original concept was for a conical nose, this evolved (after 1987?) to a flat shovel shape.[ citation needed ]

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,[ when? ] no scramjet engine was close to operational.[ citation needed ]

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.[ citation needed ]

Temperatures on the airframe were expected to be 980 °C (1,800 °F) over a large part of the surface, with maxima of more than 1,650 °C (3,000 °F) 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.[ citation needed ]

Specifications (X-30 as designed)

[ citation needed ]

General characteristics

Performance

Design and materials legacy

See also

Aircraft of comparable role, configuration, and era

Related Research Articles

<span class="mw-page-title-main">Single-stage-to-orbit</span> Launch system that only uses one rocket stage

A single-stage-to-orbit (SSTO) vehicle reaches orbit from the surface of a body using only propellants and fluids and without expending tanks, engines, or other major hardware. The term exclusively refers to reusable vehicles. To date, no Earth-launched SSTO launch vehicles have ever been flown; orbital launches from Earth have been performed by either fully or partially expendable multi-stage rockets.

<span class="mw-page-title-main">North American X-15</span> Rocket-powered aircraft and spaceplane operated by the US Air Force and NASA

The North American X-15 is a hypersonic rocket-powered aircraft operated by the United States Air Force and the National Aeronautics and Space Administration (NASA) as part of the X-plane series of experimental aircraft. The X-15 set speed and altitude records in the 1960s, crossing the edge of outer space and returning with valuable data used in aircraft and spacecraft design. The X-15's highest speed, 4,520 miles per hour, was achieved on 3 October 1967, when William J. Knight flew at Mach 6.7 at an altitude of 102,100 feet (31,120 m), or 19.34 miles. This set the official world record for the highest speed ever recorded by a crewed, powered aircraft, which remains unbroken.

<span class="mw-page-title-main">Waverider</span> Hypersonic aircraft design

A waverider is a hypersonic aircraft design that improves its supersonic lift-to-drag ratio by using the shock waves being generated by its own flight as a lifting surface, a phenomenon known as compression lift.

<span class="mw-page-title-main">Scramjet</span> Jet engine where combustion takes place in supersonic airflow

A scramjet is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in ramjets, a scramjet relies on high vehicle speed to compress the incoming air forcefully before combustion, but whereas a ramjet decelerates the air to subsonic velocities before combustion using shock cones, a scramjet has no shock cone and slows the airflow using shockwaves produced by its ignition source in place of a shock cone. This allows the scramjet to operate efficiently at extremely high speeds.

<span class="mw-page-title-main">Spaceplane</span> Spacecraft capable of aerodynamic flight in atmosphere

A spaceplane is a vehicle that can fly and glide like an aircraft in Earth's atmosphere and maneuver like a spacecraft in outer space. To do so, spaceplanes must incorporate features of both aircraft and spacecraft. Orbital spaceplanes tend to be more similar to conventional spacecraft, while sub-orbital spaceplanes tend to be more similar to fixed-wing aircraft. All spaceplanes to date have been rocket-powered for takeoff and climb, but have then landed as unpowered gliders.

<span class="mw-page-title-main">NASA X-43</span> Unmanned US experimental hypersonic aircraft, 1991-2000

The NASA X-43 was an experimental unmanned hypersonic aircraft with multiple planned scale variations meant to test various aspects of hypersonic flight. It was part of the X-plane series and specifically of NASA's Hyper-X program developed in the late 1990s. It set several airspeed records for jet aircraft. The X-43 is the fastest jet-powered aircraft on record at approximately Mach 9.6.

<span class="mw-page-title-main">Lockheed Martin X-33</span> Uncrewed re-usable spaceplane technology demonstrator for the VentureStar

The Lockheed Martin X-33 was a proposed uncrewed, sub-scale technology demonstrator suborbital spaceplane that was developed for a period in the 1990s. The X-33 was a technology demonstrator for the VentureStar orbital spaceplane, which was planned to be a next-generation, commercially operated reusable launch vehicle. The X-33 would flight-test a range of technologies that NASA believed it needed for single-stage-to-orbit reusable launch vehicles, such as metallic thermal protection systems, composite cryogenic fuel tanks for liquid hydrogen, the aerospike engine, autonomous (uncrewed) flight control, rapid flight turn-around times through streamlined operations, and its lifting body aerodynamics.

<span class="mw-page-title-main">Blackstar (spacecraft)</span> Reported codename of a secret U.S. orbital spaceplane system

Blackstar is the reported code-name of a secret United States orbital spaceplane system. The possible existence of the Blackstar program was reported in March 2006 by Aviation Week & Space Technology magazine; the magazine reported that the program had been underway since at least the early 1990s, and that the impetus for Blackstar was to allow the United States government to retain orbital reconnaissance capabilities jeopardized following the 1986 Challenger disaster. The article also said that the United States Air Force's Space Command was unaware of Blackstar, suggesting it was operated by an intelligence agency such as the National Reconnaissance Office.

<span class="mw-page-title-main">Boeing X-51 Waverider</span> Unmanned hypersonic experimental aircraft

The Boeing X-51 Waverider is an unmanned research scramjet experimental aircraft for hypersonic flight at Mach 5 and an altitude of 70,000 feet (21,000 m). The aircraft was designated X-51 in 2005. It completed its first powered hypersonic flight on 26 May 2010. After two unsuccessful test flights, the X-51 completed a flight of over six minutes and reached speeds of over Mach 5 for 210 seconds on 1 May 2013 for the longest duration powered hypersonic flight.

Scramjet programs refers to research and testing programs for the development of supersonic combustion ramjets, known as scramjets. This list provides a short overview of national and international collaborations, and civilian and military programs. The USA, Russia, India, and China (2014), have succeeded at developing scramjet technologies.

<span class="mw-page-title-main">Lockheed L-301</span>

Lockheed L-301 was an experimental air-breathing hypersonic aircraft project. It was developed by the NASA and United States Air Force (USAF) organization National Hypersonic Flight Research Facility, with Skunk Works as the prime contractor. In January 1977, the program was "tentatively scheduled to operate two vehicles for eight years and to conduct 100 flights per vehicle." NASA discontinued work on L-301 and NHRF in September 1977 due to budget constraints and lack of need.

<span class="mw-page-title-main">Tupolev Tu-2000</span> Russian hypersonic aircraft

The Tupolev Tu-2000 was a planned hypersonic flight experimental aircraft designed by the Tupolev design bureau. It was intended to test technologies for a single-stage-to-orbit aerospaceplane and also the Tupolev Tu-360 intercontinental bomber.

<span class="mw-page-title-main">Hypersonic flight</span> Flight at altitudes lower than 90km (56 mi) and at speeds above Mach 5

Hypersonic flight is flight through the atmosphere below altitudes of about 90 km (56 mi) at speeds greater than Mach 5, a speed where dissociation of air begins to become significant and high heat loads exist. Speeds over Mach 25 have been achieved below the thermosphere as of 2020.

<span class="mw-page-title-main">Ayaks</span> Russian hypersonic aircraft program

The Ayaks is a hypersonic waverider aircraft program started in the Soviet Union and currently under development by the Hypersonic Systems Research Institute (HSRI) of Leninets Holding Company in Saint Petersburg, Russia.

<span class="mw-page-title-main">14-X</span> Brazilian scramjet engine in development

The 14-X is a Brazilian scramjet engine in development by the Aerothermodynamics and Hypersonics Laboratory Henry T. Nagamatsu of the Institute of Advanced Studies (IEAv) of the Department of Aerospace Science and Technology as part of the PropHiper. The name is a reference to the 14-bis, of the Brazilian inventor and aviation pioneer Alberto Santos-Dumont.

HyShot is a research project of The University of Queensland, Australia Centre for Hypersonics, to demonstrate the possibility of supersonic combustion under flight conditions using two scramjet engines, one designed by The University of Queensland and one designed by QinetiQ.

Frederick Stucky Billig was an American aerospace engineer who was a pioneer in the development of scramjet propulsion.

<span class="mw-page-title-main">Hypersonic Technology Demonstrator Vehicle</span> Hypersonic demonstration aircraft

The HSTDV is an unmanned scramjet demonstration aircraft for hypersonic flight. It is being developed as a carrier vehicle for hypersonic and long-range cruise missiles, and will have multiple civilian applications including the launching of small satellites at low cost. The HSTDV program is being run by the Defence Research and Development Organisation (DRDO).

<span class="mw-page-title-main">Lockheed Martin SR-72</span> US Air Force hypersonic aircraft concept

The Lockheed Martin SR-72, colloquially referred to as "Son of Blackbird", is an American hypersonic UAV concept intended for intelligence, surveillance and reconnaissance (ISR) proposed privately in 2013 by Lockheed Martin as a successor to the retired Lockheed SR-71 Blackbird. In 2018, company executives said an SR-72 test vehicle could fly by 2025 and enter service in the 2030s.

References

  1. 1 2 3 Chang, Kenneth (October 20, 2014). "25 Years Ago, NASA Envisioned Its Own 'Orient Express'". The New York Times . Retrieved October 21, 2014.
  2. 1 2 3 4 5 "National Aero-Space Plane Program Fact Sheet". TOTSE . Archived from the original on April 2, 2016. Retrieved November 2, 2023.
  3. Andersen, Drucella; Baker, Sue; Sandy, Mary (November 4, 1991). "Mississippi State Wins Aero-Space Plane Mockup Competition". NASA. Archived from the original on December 5, 2007. Retrieved November 2, 2023.
  4. "History: NASP X-30". Raspet Flight Research Laboratory. Archived from the original on March 17, 2005. Retrieved November 2, 2023.
  5. Andersen, Drucella (June 10, 1992). "X-30 National Aero-Space Plane Mockup Rolls Out". NASA. Archived from the original on September 3, 2009. Retrieved November 2, 2023.
  6. Visible on Google Maps at 34.709610, -86.642011 ( https://www.google.com/maps/place/34%C2%B042'41.0%22N+86%C2%B039'15.0%22W/@34.7095563,-86.6420974,61m/data=!3m1!1e3!4m4!3m3!8m2!3d34.711389!4d-86.654167?hl=en&entry=ttu&g_ep=EgoyMDI0MTAwOC4wIKXMDSoASAFQAw%3D%3D )