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  2. Single-stage-to-orbit - Wikipedia

    en.wikipedia.org/wiki/Single-stage-to-orbit

    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. The main projected advantage of the SSTO concept is elimination of the hardware replacement inherent in expendable launch systems.

  3. McDonnell Douglas DC-X - Wikipedia

    en.wikipedia.org/wiki/McDonnell_Douglas_DC-X

    The DC-X, short for Delta Clipper or Delta Clipper Experimental, was an uncrewed prototype of a reusable single-stage-to-orbit launch vehicle built by McDonnell Douglas in conjunction with the United States Department of Defense's Strategic Defense Initiative Organization (SDIO) from 1991 to 1993.

  4. Douglas SASSTO - Wikipedia

    en.wikipedia.org/wiki/Douglas_SASSTO

    Douglas Aircraft's SASSTO, short for "Saturn Application Single Stage to Orbit", was a single-stage-to-orbit (SSTO) reusable launch system designed by Philip Bono's team in 1967. SASSTO was a study in minimalist designs, a launcher with the specific intent of repeatedly placing a Gemini capsule in orbit for the lowest possible cost.

  5. Skylon (spacecraft) - Wikipedia

    en.wikipedia.org/wiki/Skylon_(spacecraft)

    Skylon has its origins within a previous space development programme for an envisioned single-stage-to-orbit (SSTO) spaceplane, known as HOTOL. [14] In 1982, when work commenced on the HOTOL by several British companies, there was significant international interest to develop and produce viable reusable launch systems, perhaps the most high-profile of these being the NASA-operated Space Shuttle.

  6. Lockheed Martin X-33 - Wikipedia

    en.wikipedia.org/wiki/Lockheed_Martin_X-33

    Doing away with the need for "staging" with launch vehicles, such as with the Shuttle and the Apollo rockets, would lead to an inherently more reliable and safer space launch vehicle. While the X-33 would not approach airplane-like safety, the X-33 would attempt to demonstrate 0.997 reliability, or 3 mishaps out of 1,000 launches, which would ...

  7. British Aerospace HOTOL - Wikipedia

    en.wikipedia.org/wiki/British_Aerospace_HOTOL

    Designed as a single-stage-to-orbit (SSTO) reusable winged launch vehicle, HOTOL was to be fitted with a unique air-breathing engine, the RB545 or Swallow, that was under development by British engine manufacturer Rolls-Royce.

  8. Kankoh-maru - Wikipedia

    en.wikipedia.org/wiki/Kankoh-maru

    The Kankoh-maru (観光丸, Kankōmaru) is a proposed vertical takeoff and landing (VTVL), single-stage-to-orbit (SSTO), reusable launch system (rocket-powered spacecraft). According to a document from July 1997, it would have been manufactured by Kawasaki Heavy Industries and Mitsubishi Heavy Industries, with its formal name being the Kawasaki ...

  9. List of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/List_of_orbital_launch_systems

    ISRO's launch vehicles. Left to right: SLV, ASLV, PSLV, GSLV, LVM3 RLV Human Rated Launch Vehicle (HRLV) Vikram series, the under development orbital class launch family of Skyroot Aerospace in comparison with already flown Vikram S, the sounding rocket ISRO/DoS systems. SLV-3 – Retired; Augmented Satellite Launch Vehicle (ASLV) – Retired