Английская Википедия:Hypersonic glide vehicle

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Файл:DF-17 Missile 20221020.jpg

Chinese DF-ZF hypersonic glide vehicle mounted on the DF-17 ballistic missile.

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 missiles to significantly change their trajectories after launch. The concept of HGVs is similar to MaRVs, but HGVs are separated from their rocket boosters shortly after launch as opposed to MaRVs which can only maneuver just before the impact. Conventional ballistic missiles follow a predictable ballistic trajectory and are vulnerable to interception by the latest anti-ballistic missile (ABM) systems. The in-flight maneuverability of HGVs makes them unpredictable, allowing them to effectively evade air defenses. Шаблон:As of, hypersonic glide vehicles are the subject of an arms race.

Projects

• DF-ZF (developed and deployed) / Mach 5–10

• VERAS (program launched in 1965 and cancelled in 1971)
• VMaX (first flight test took place on June 26, 2023 from the DGA's site in Biscarrosse and was successful)
• VMaX-2 (under development; first flight test expected in 2024 or 2025)

• HGV-202F (under development)

• Fattah-2 Mach 13-15

Файл:موشک هایپرسونیک فتاح2.jpg

Iranian Fattah-2

• Hyper Velocity Gliding Projectile (HVGP) (under development)

• The Avangard (developed and deployed)/Mach 27-28

• Hypersonic Technology Vehicle 2 (experimental)
• AGM-183 Air-launched Rapid Response Weapon (ARRW) (under development)
• OpFires (under development)
• Common-Hypersonic Glide Body (C-HGB) (in development for US Army (LRHW) and US Navy Conventional Prompt Strike (CPS))

Countermeasures

Boost-glide weapons are generally designed to avoid existing missile defense systems, either by continually maneuvering or by flying at lower altitudes to reduce warning time. This generally makes such weapons easier to intercept using defensive systems intended for lower-altitude "low-tier" targets. Flying at lower speeds than short-range ballistic missile warheads makes them easier to attack. Those that approach with very low terminal attack profiles are even subject to attack by modern hypervelocity guns and railguns.

Russian sources claim that its Avangard HGV travels at Mach 27 and "constantly changes its course and altitude while it flies through the atmosphere, chaotically zigzagging on its path to its target, making it impossible to predict the weapon's location", thus making it supposedly "invulnerable to interception". However these claims are problematic as hypersonic glide vehicles suffer from several known issues. Due to their speed, an envelope of ionized gas forms around the glide vehicle in atmosphere, making base-to-vehicle communication impossible. This cloud of ionized gas is easy for satellites to detect and track. Furthermore, the heat generated at those velocities renders external sensors inoperable and necessitates the detachment of HGVs from their carrier ballistic missiles at the upper limits of the atmosphere to avoid their burning up.

Hypersonics, like the Avangard HGV, generally use scramjet engines to achieve hypersonic speeds. Scramjet engines function only when the glide vehicle reaches mach 4.5. These engines are disengaged as the HGV enters the terminal phase of its flight. Failure to deactivate the engines would cause a catastrophic build up of heat in the vehicle as the atmosphere becomes denser during reentry, prematurely destroying the vehicle. Therefore, the terminal phase of an HGV's re-entry is similar to that of a multiple independently targetable reentry vehicle. For instance, the Avangard would not hit its target while "zig-zagging" at Mach 27, but rather would impact at a velocity under Mach 4 and on a linear trajectory.Шаблон:Citation needed The superior evasion capabilities that HGVs employ are largely limited to the upper atmospheric flight span.

See also

• Hypersonic flight
• Hypersonic weapon
• Maneuverable reentry vehicle
• Multiple independently targetable reentry vehicle
• Non-ballistic atmospheric entry