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The Advanced Maneuverable Reentry Vehicle (AMaRV) was a prototype MARV built by McDonnell Douglas. Four AMaRVs were made and represented a significant leap in reentry vehicle sophistication. Three of the AMaRVs were launched by Minuteman-1 ICBMs on 20 December 1979, 8 October 1980 and 4 October 1981.
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] This research was eventually put to use in the Pershing II's MARV reentry vehicle. In this case, there is no extended gliding phase; the warhead uses lift only for short periods to adjust its ...
4. About 180 seconds after launch, the third-stage thrust terminates and the post-boost vehicle (D) separates from the rocket. 5. The post-boost vehicle maneuvers itself and prepares for re-entry vehicle (RV) deployment. 6. While the post-boost vehicle backs away, the RVs, decoys, and chaff are deployed (this may occur during ascent). 7.
Prototype of the Mk-2 Reentry Vehicle (RV), based on blunt body theory. The original American sphere-cone aeroshell was the Mk-2 RV (reentry vehicle), which was developed in 1955 by the General Electric Corp. The Mk-2's design was derived from blunt-body theory and used a radiatively cooled thermal protection system (TPS) based upon a metallic ...
Original file (1,275 × 1,650 pixels, file size: 44.01 MB, MIME type: application/pdf, 160 pages) This is a file from the Wikimedia Commons . Information from its description page there is shown below.
Agni-VI is expected to have Multiple independently targetable reentry vehicle as well as Maneuverable reentry vehicle (MaRV). [10] And these maneuverable warheads will give Agni VI an extended range exact figure of which is currently classified. [5] It will be taller than its predecessor Agni V, and was expected to be flight tested by 2017. [5]
Maneuvering reentry vehicles MARV (instead of symmetrically shaped warheads) induce lateral drag during reentry and hence strongly bend the trajectory, thus deceiving lower altitude interceptor systems that generally assume a straight decelerating trajectory and which have a limited terminal guidance maneuverability and course correction ...
Its payload is believed to be 600 kg (1,300 lb) with a range of 900 km (560 mi) and improved accuracy of 30–45 m CEP. The DF-15B is a further upgraded variant with similar features, as well as an active radar seeker, laser rangefinder, and maneuverable reentry vehicle. It is capable of ranges between 50–800 km (31–497 mi) with greater ...
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