| C-101 | |
|---|---|
| Type | anti-ship, and air to surface cruise missile |
| Place of origin | China |
| Service history | |
| Used by | China |
| Production history | |
| Manufacturer | China Aerospace Science and Industry Corporation |
| Specifications | |
| Mass | 1.85 t (ship launched) 1.5 t (air-launched) |
| Length | 6.5 m (ship launched) 7.5 m (air-launched) |
| Diameter | 0.54 m |
| Wingspan | 1.62 m |
| Warhead | 300 kg warhead |
Detonation mechanism | Semi-armor-piercing |
| Engine | Ramjet |
| Propellant | Kerosene |
Operational range | 50 km |
| Flight altitude | 50 m (cruising) 5 m (terminal) |
| Maximum speed | Mach 2 |
Guidance system | Radar |
Launch platform | Air, surface |
The C-101 is a Chinese supersonic anti-ship cruise missile. It is manufactured by the China Aerospace Science and Industry Corporation Third Academy.
The C-101 was an early Chinese supersonic cruise missile. It has been described as unsuccessful.
The People's Liberation Army Navy designation is YJ-1 (Chinese: 鹰击-1; pinyin: yingji-1; lit. 'eagle strike 1'; NATO reporting name: CSS-X-5).
The C-101 is launched with solid-fuel rocket boosters to a speed of Mach 1.8. Two ramjets sustain a cruise and impact speed of Mach 2. At three kilometers from the target, the missile descends from a cruise altitude of 50 meters to 5 meters.