Checkpoint (missile): Difference between revisions
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Created page with "{{Nouvelle Alexandrie Article}} {{ infobox | bodyclass = toccolours | bodystyle = float:right; margin: 0 0 1em 1em; font-size: 85%; width: 30em;background-color:#C0C0C0;..." |
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| data6 = Aircraft | | data6 = Aircraft | ||
| label7 = Guidance | | label7 = Guidance | ||
| data7 = Astro-inertial, | | data7 = Astro-inertial, [[NovaNav MPS|MPS]] | ||
| label8 = Weight | | label8 = Weight | ||
| data8 = 1,000 kg cruiser, 2,300 kg with booster | | data8 = 1,000 kg cruiser, 2,300 kg with booster | ||
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}} | }} | ||
[[Category: | [[Category:Missiles]] | ||
[[Category:Javelin Industries]] | |||
Latest revision as of 22:26, 4 June 2025
| JAV 100 Checkpoint | |
| Type | Hypersonic cruise missile |
|---|---|
| Place of origin |
 Nouvelle Alexandrie |
| Designed | Javelin Industries |
| Manufacturer | Javelin Industries |
| Launch platform | Aircraft |
| Guidance | Astro-inertial, MPS |
| Weight | 1,000 kg cruiser, 2,300 kg with booster |
| Length | 4.5 m cruiser, 7.0 m with booster |
| Diameter | 0.6 m |
| Warhead | 250 kg unitary penetrator |
| Propulsion | Dual mode scramjet (sustainer), solid fuel rocket (booster) |
| Speed | Mach 8.0 |
| Cruise altitude | 30,000 m |
| Range | 2,500 km |
