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1. en.wikipedia.org › wiki › Martin_Marietta_X-24Martin Marietta X-24 - Wikipedia

   en.wikipedia.org › wiki › Martin_Marietta_X-24

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   The SV-5J was a jet-powered version of the rocket-powered X-24A. The SV-5J had identical dimensions to the X-24A, but was powered by a single Pratt & Whitney J60-PW-1 jet engine of 1360 kgf, in place of the X-24A's Reaction Motors XLR-11-RM-13 rocket engine.

2. nationalinterest.org › blog › buzzX-24C: The Air Force's 50-Year-Old Hypersonic Scramjet Aircraft

   nationalinterest.org › blog › buzz

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   18 lis 2023 · The scramjet engine would propel the X-24C at sustained speeds in excess of Mach 6, reaching intended peak speeds that were higher than Mach 8, or more than 6,130 miles per hour.

3. www.lockheedmartin.com › en-us › newsControlling Descent From on High: The X-24 - Lockheed Martin

   www.lockheedmartin.com › en-us › news

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   A closer looked revealed that it was a teardrop-shaped aircraft—without wings. It descended—as if in a state of free-fall—until its pilot, Jerauld Gentry, ignited a rocket engine, propelling the strange vehicle higher into the sky at speeds approaching Mach 1.

4. theaviationgeekclub.com › faster-than-the-x-15-the-never-told-story-of-theFaster than the X-15: the never told story of the Lockheed X 24C...

   theaviationgeekclub.com › faster-than-the-x-15-the-never-told-story-of-the

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   30 maj 2021 · This rocket engine, burning RP-1 and liquid oxygen (LOX), was intended to accelerate the X-24C to hypersonic speeds in order to ignite the hydrogen-fueled, air-breathing ram/scramjet (supersonic-combustion ramjet) mounted in the belly of the airframe with which it would attain cruise speeds of at least Mach 6 and peak velocities of Mach 8+ at ...

5. ntrs.nasa.gov › citations › 19790008668Configuration development study of the X-24C hypersonic research...

   ntrs.nasa.gov › citations › 19790008668

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   The X-24C Hypersonic Research Vehicle, configured with a heat-sink structure, a launch mass limit of 31.75 Mg and powered by an LR-105 Rocket Engine plus 12 LR-101 Sustainer Engines, was found to be the more cost effective of the candidate configurations.

6. thehighfrontier.blog › 2017/05/16 › flying-without-wings-the-martin-sv-5x-24Flying Without Wings: The Martin SV-5/X-24 Lifting Bodies

   thehighfrontier.blog › 2017/05/16 › flying-without-wings-the-martin-sv-5x-24

   16 maj 2017 · Acting as a testbed for interchangeable scramjet prototypes the X-24C would be capable of speeds in the range of Mach 6-8, effectively picking up where the X-15A-2 had left off.

7. ntrs.nasa.gov › citations › 19790008669Configuration development study of the X-24C hypersonic research...

   ntrs.nasa.gov › citations › 19790008669

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   The conclusion evolved from the three phased study on the configuration development of the X-24C Hypersonic Research Airplane makes it evident that it is practical to design and build the high performance National Hypersonic Flight Research Facility airplane with today's state of the art within the cost and operational constraints established ...