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At a glance
CJ-1000 (missile)larger figure on 1 of 1
Sea Skualarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | CJ-1000 (missile) | Sea Skua |
|---|---|---|
| Type | Land-attack hypersonic cruise missile[source] | Air-to-surface missile , anti-ship missile[source] |
| Place of origin | China[source] | United Kingdom[source] |
| Used by | People's Liberation Army Rocket Force[source] | See operators[source] |
| Engine | scramjet engine[source] | Solid fuel booster / solid fuel sustainer |
Wingspan
Single source0.72 m[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Launch platform | Transporter erector launcher[source] | Westland Lynx, Combattante BR-42 FAC[source] |
|---|
| In service | — | 1982[source] |
|---|
| Wars | — | Falklands War Gulf War[source] |
|---|
| Designer | — | British Aircraft Corporation[source] |
|---|
| Designed | — | 1972[source] |
|---|
| Manufacturer | — | British Aircraft Corporation (1972–1977) BAe Dynamics (1977–1999) MBDA (UK) Ltd (since 1999)[source] |
|---|
| Produced | — | 1975[source] |
|---|
| Warhead | — | 30 kg semi armour piercing, 9 kg RDX[source] |
|---|
| Detonation mechanism | — | Impact fuze, delayed detonation[source] |
|---|
| Guidance system | — | Semi-active radar homing[source] |
|---|
| Steering system | — | Control surfaces[source] |
|---|
| Reported operators |
| — |
|---|