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  2. RIM-161 Standard Missile 3 - Wikipedia

    en.wikipedia.org/wiki/RIM-161_Standard_Missile_3

    The RIM-161 Standard Missile 3 (SM-3) is a ship-based surface-to-air missile used by the United States Navy to intercept ballistic missiles as a part of Aegis Ballistic Missile Defense System. [ 5 ] [ 6 ] Although primarily designed as an anti-ballistic missile , the SM-3 has also been employed in an anti-satellite capacity against a satellite ...

  3. Multiple independently targetable reentry vehicle - Wikipedia

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

    With single-warhead missiles, one missile must be launched for each target. By contrast, with a MIRV warhead, the post-boost (or bus) stage can dispense the warheads against multiple targets across a broad area. Reduces the effectiveness of an anti-ballistic missile system that relies on intercepting individual warheads. [16]

  4. Arrow 3 - Wikipedia

    en.wikipedia.org/wiki/Arrow_3

    The Arrow 3 or Hetz 3 (Hebrew: חֵץ 3, pronounced or pronounced) is an exoatmospheric hypersonic anti-ballistic missile, jointly funded, developed and produced by Israel and the United States. Undertaken by Israel Aerospace Industries (IAI) and Boeing , it is overseen by the Israeli Ministry of Defense's " Homa " ( Hebrew : חומה ...

  5. List of missiles - Wikipedia

    en.wikipedia.org/wiki/List_of_missiles

    R-5 Pobeda theatre ballistic missile (SS-3 Shyster) R-7 Semyorka intercontinental ballistic missile (USSR/Russia; Cold War) (NATO name SS-6 Sapwood) R-9 Desna intercontinental ballistic missile (USSR/Russia; Cold War) (NATO name SS-8 Sasin) R-11 Zemlya tactical ballistic missile (USSR; Cold War) (NATO name SS-1b Scud)

  6. Ballistic missile flight phases - Wikipedia

    en.wikipedia.org/wiki/Ballistic_missile_flight...

    The boost phase is the portion of the flight of a ballistic missile or space vehicle during which the booster and sustainer engines operate until it reaches peak velocity. . This phase can take 3 to 4 minutes for a solid rocket (shorter for a liquid-propellant rocket), the altitude at the end of this phase is 150–200 km, and the typical burn-out speed is 7 k

  7. Ballistic missile - Wikipedia

    en.wikipedia.org/wiki/Ballistic_missile

    The type of ballistic missile with the greatest range is an intercontinental ballistic missile (ICBM). The largest ICBMs are capable of full orbital flight . These missiles are in a distinct category from cruise missiles , which are aerodynamically guided in powered flight and thus restricted to the atmosphere.

  8. UDOP - Wikipedia

    en.wikipedia.org/wiki/UDOP

    The UDOP (UHF Doppler) multistatic radar and multiradar system (MSRS) utilizes Doppler radar for missile tracking and trajectory measurement. A target is illuminated at 450 MHz. Five receiving stations, located along the baselines with the lengths from 40 to 120 km (25 to 75 mi), receive signals from the target's transponder at 900 MHz.

  9. Sayyad (missile) - Wikipedia

    en.wikipedia.org/wiki/Sayyad_(missile)

    Sayyad-3 is a similar missile, but with a long-range capability. It has a similar diameter as Sayyad-2 but a longer body with different wings and control surfaces. Based on current estimates Sayyad-3 has a range of about 150–200 km. [10] Iranian Defence Minister Hossein Dehghan stated the maximum range is about 120 km. [11] This missile will be added to SAM systems via the TALASH-3 system. [12]