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  2. Hypersonic and Ballistic Tracking Space Sensor - Wikipedia

    en.wikipedia.org/wiki/Hypersonic_and_Ballistic...

    The current phase of the HBTSS program is in protype stage and lacks operational capability. [1] The HBTSS program plans to launch two demonstration sensors into orbit by Fiscal Year (FY) 2023. [ 1 ] The Missile Defense Agency have selected two military contractors - L3Harris Technologies and Northrop Grumman - to design, build, and lastly ...

  3. Autonetics - Wikipedia

    en.wikipedia.org/wiki/Autonetics

    Autonetics also developed and tested flight programs for the D37D Minuteman III computer. The 1966 Autonetics DDA integrator was the first MOS large scale array (LSA) using four-phase logic . After producing the DDA and other MOS-LSA circuits, the team involved decided to design a general purpose computer suitable for navigation (sometimes ...

  4. Aeroprediction - Wikipedia

    en.wikipedia.org/wiki/Aeroprediction

    The Aeroprediction Code is a semi-empirical computer program that estimates the aerodynamics of weapons over the Mach number range 0 to 20, angle of attack range 0 to 90 degrees, and for configurations that have various cross sectional body shapes.

  5. Missile Datcom - Wikipedia

    en.wikipedia.org/wiki/Missile_Datcom

    Missile DATCOM is a widely used semi-empirical datasheet component build-up method for the prediction of missile aerodynamic coefficients. It is an example of an engineering aeroprediction method which can be used to generate an aerodynamic database of the vehicle’s aerodynamic coefficients at various flight conditions.

  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. Missile guidance - Wikipedia

    en.wikipedia.org/wiki/Missile_guidance

    In World War II, guided missiles were first developed, as part of the German V-weapons program. [2] Project Pigeon was American behaviorist B.F. Skinner's attempt to develop a pigeon-guided bomb. The first U.S. ballistic missile with a highly accurate inertial guidance system was the short-range PGM-11 Redstone. [3]

  8. Conventional Prompt Strike - Wikipedia

    en.wikipedia.org/wiki/Conventional_Prompt_Strike

    On 18 November 2011, the first advanced hypersonic weapon (AHW) glide vehicle was successfully tested by the U.S. Army Space and Missile Defense Command as part of the Prompt Global Strike program. [citation needed] The missile was launched from the Pacific Missile Range Facility in Hawaii, and struck a target at the Reagan Test Site on ...

  9. M270 Multiple Launch Rocket System - Wikipedia

    en.wikipedia.org/wiki/M270_Multiple_Launch...

    M57 (ATACMS TACMS 2000) missile with GPS-aided guidance. The missile carries the same WAU-23/B warhead section as the M48. Range: 70–300 kilometres (43–186 mi). 513 M57 were produced between 2004 and 2013. [64] [55] M57E1 (ATACMS Modification (MOD) missile with GPS-aided guidance. The M57E1 is the designation for upgraded M39 and M39A1 with ...