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Kh-90
Russian hypersonic cruise missile
Russian hypersonic cruise missile
| Field | Value |
|---|---|
| is_missile | yes |
| name | Kh-90 GELA |
| (NATO reporting name: AS-X-21) | |
| image | Experimental hypersonic aircraft layout during the "Armiya 2021" exhibition.jpg |
| origin | Russia |
| type | Air-launched Hypersonic weapon |
| manufacturer | MKB Raduga, Turaevo TMKB Soyuz, TsAGI |
| propellant | solid propellant booster, liquid ramjet (or scramjet), kerosene |
| engine | booster + Ramjet Raduga TMKB Soyuz (or Scramjet ?) TsAGI |
| weight | 15 metric tons |
| length | 11 m |
| diameter | 0.8 - 0.9m |
| wingspan | 7m |
| speed | Mach 5+ |
| filling | various: HE, FAE, TBX, two nuclear each 1.2 Mt |
| filling_weight | 200 kg to |
| guidance | inertial, TERCOM , GLONASS , Radar , IR IIR , TV camera , Opto-Electronic , CCD |
| launch_platform | Aircraft, can be loaded on ship ground TEL, maybe submarine |
(NATO reporting name: AS-X-21)
The Kh-90 GELA (, Hypersonic Experimental Flight Vehicle) is a Soviet/Russian air-to-surface hypersonic missile. It was supposed to replace subsonic intermediate range missiles in the Soviet inventory. The missile was an ambitious project, as the main objective was to develop it into a hypersonic missile. It was to be a successor to the Kh-45, which never entered service.
The missile was designed by Raduga. It was equipped with a one-megaton thermonuclear warhead and used inertial navigation with mid-course update via data link. It had a maximum range of 3,000 km.
It was developed at the beginning of 1980, following the Kh-80 and Kholod projects. It was shown to the public an MAKS Airshow 1995.
References
References
- Karnozov, Vladimir. "Putin Reveals Zircon Mach 9 Missile Specification".
- "Гиперзвуковая ракета СССР Х-90 Гэла".
- "Гиперзвуковая ракета СССР Х-90 Гэла".
- "В России создана гиперзвуковая ракета".
- "Стратегическая крылатая ракета 3М-25 Метеорит (П-750 Гром ) - Ракетная техника".
- "Х-90 ГЭЛА".
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