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  2. Atmospheric entry - Wikipedia

    en.wikipedia.org/wiki/Atmospheric_entry

    Early reentry-vehicle concepts visualized in shadowgraphs of high speed wind tunnel tests. The concept of the ablative heat shield was described as early as 1920 by Robert Goddard: "In the case of meteors, which enter the atmosphere with speeds as high as 30 miles (48 km) per second, the interior of the meteors remains cold, and the erosion is due, to a large extent, to chipping or cracking of ...

  3. Non-ballistic atmospheric entry - Wikipedia

    en.wikipedia.org/wiki/Non-ballistic_atmospheric...

    The primary goal was to have the RV change its path during reentry so that anti-ballistic missiles (ABMs) would not be able to track their movements rapidly enough for a successful interception. The first known example was the Alpha Draco tests of 1959, followed by the Boost Glide Reentry Vehicle (BGRV) test series, ASSET [16] and PRIME. [17]

  4. Reentry capsule - Wikipedia

    en.wikipedia.org/wiki/Reentry_capsule

    Soyuz TMA reentry capsule after landing, 2005. A reentry capsule is the portion of a space capsule which returns to Earth following a spaceflight. The shape is determined partly by aerodynamics; a capsule is aerodynamically stable falling blunt end first, which allows only the blunt end to require a heat shield for atmospheric entry. A crewed ...

  5. Harry Julian Allen - Wikipedia

    en.wikipedia.org/wiki/Harry_Julian_Allen

    Allen was interested in the full range of aerodynamics research, and made contributions to the study of subsonic, transonic, supersonic and hypersonic flow. [2] When the United States became interested in the design of ballistic missiles, Allen began research in the dynamics and thermodynamics of atmospheric reentry, as well as the effects of radiation and meteorites on space vehicles.

  6. Maneuverable reentry vehicle - Wikipedia

    en.wikipedia.org/wiki/Maneuverable_reentry_vehicle

    The maneuverable reentry vehicle (abbreviated MARV or MaRV) is a type of warhead for ballistic missiles that is capable of maneuvering and changing its trajectory. There are two general reasons to use MARV. One is to make it more difficult to track the re-entry vehicle (RV) and

  7. Hypersonic glide vehicle - Wikipedia

    en.wikipedia.org/wiki/Hypersonic_glide_vehicle

    Chinese DF-ZF hypersonic glide vehicle mounted on the DF-17 ballistic missile. American Long-Range Hypersonic Weapon being deployed at the Cape Canaveral Space Force Station. A hypersonic glide vehicle (HGV) is a type of warhead for ballistic missiles that can maneuver and glide at hypersonic speed. It is used in conjunction with ballistic ...

  8. Ballistic coefficient - Wikipedia

    en.wikipedia.org/wiki/Ballistic_coefficient

    The ballistic coefficient of an atmospheric reentry vehicle has a significant effect on its behavior. A very high ballistic coefficient vehicle would lose velocity very slowly and would impact the Earth's surface at higher speeds. In contrast, a low ballistic coefficient vehicle would reach subsonic speeds before reaching the ground. [75]

  9. Multiple independently targetable reentry vehicle - Wikipedia

    en.wikipedia.org/wiki/Multiple_independently_tar...

    A multiple independently targetable reentry vehicle (MIRV) is an exoatmospheric ballistic missile payload containing several warheads, each capable of being aimed to hit a different target. The concept is almost invariably associated with intercontinental ballistic missiles carrying thermonuclear warheads , even if not strictly being limited to ...