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HGV-202F a hypersonic Boost-glide vehicle is being designed, developed, and manufactured by an Indian Defense and Space company HTNP Industries. [citation needed] It is designed to be mounted on a Agni-V and Agni-VI, a type of ballistic missile specifically designed to carry HGVs.
China. Chinese DF-ZF hypersonic glide vehicle mounted on the DF-17 ballistic missile.. DF-ZF (developed and deployed) / Mach 5–10 [5]; GDF-600 (concept) In addition to a unified payload the Guangdong Aerodynamic Research Academy claims to be exploring fitting the conceptual weapon with various submunitions including what it calls a patrol projectile.
The HGV can perform terminal maneuvers and follow highly complex and adaptive flight paths. It has a demonstrated range of at least 1,500 km (930 mi). The missile will have several warhead configurations for use in various roles by all the branches of the Indian Armed Forces. [4] [24] [27] LRAShM is cold-launched from a hermetically sealed ...
Scramjet-powered aircraft (1 C, 12 P) Spaceplanes (6 C, 63 P) Pages in category "Hypersonic aircraft" ... HGV-202F; Hypersonic Technology Demonstrator Vehicle; Hyper-A;
Comparison of Ballistic Missile and Hypersonic Glide Vehicle (C-HGB) Flight Trajectories for the LRHW Program Scramjet-powered hypersonic cruise missile. A hypersonic weapon is a weapon capable of travelling at hypersonic speed, defined as above Mach 5, or above 5 times the speed of sound.
Jan. 3—Construction on the Ka Haku by Hilton Club, a 32-story timeshare tower in the heart of Waikiki at the former King's Village site, has started again after a lengthy COVID-19 hiatus.
The 1-metric-ton, 5.6-meter-long (18 ft) air vehicle under construction features a flattened octagonal cross section with mid-body stub-wings and raked tail fins and a 3.7-meter rectangular section air intake. The scramjet engine is located under the mid-body, with the aftbody serving as part of the exhaust nozzle.
The first manufactured object to achieve hypersonic flight was the two-stage Bumper rocket, consisting of a WAC Corporal second stage set on top of a V-2 first stage. In February 1949, at White Sands, the rocket reached a speed of 8,290 km/h (5,150 mph), or about Mach 6.7. [2]