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The Ares V (formerly known as the Cargo Launch Vehicle or CaLV) was the planned cargo launch component of the cancelled NASA Constellation program, which was to have replaced the Space Shuttle after its retirement in 2011. Ares V was also intended to carry supplies for a human presence on Mars. Ares V and the smaller Ares I were named after Ares, the…
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ares would space launch nasa rocket vehicle stage earth constellation moon orbit shuttle program missions used cargo also planned system
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Ares V | Burn time | 126 seconds | 1.00 | infobox |
| Ares V | Country of origin | United States | 1.00 | infobox |
| Ares V | Diameter | 8.4 or 10 m (28 or 33 ft) | 1.00 | infobox |
| Ares V | Diameter | 3.7 m (12 ft) | 1.00 | infobox |
| Ares V | Empty mass | 140,000 kg (310,000 lb) | 1.00 | infobox |
| Ares V | Function | Super heavy-lift launch vehicle | 1.00 | infobox |
| Ares V | Gross mass | 730,000 kg (1,600,000 lb) | 1.00 | infobox |
| Ares V | Gross mass | 1,914,000 kg (4,220,000 lb) | 1.00 | infobox |
| Ares V | Height | 109 or 116 m (358 or 381 ft) | 1.00 | infobox |
| Ares V | Height | 54 m (177 ft) | 1.00 | infobox |
| Ares V | Launch sites | Kennedy, LC-39A (planned) | 1.00 | infobox |
| Ares V | Mass | 3,700,000 kilograms (8,200,000 lb) | 1.00 | infobox |
| Ares V | Mass | 188,000 kg (414,000 lb) | 1.00 | infobox |
| Ares V | Mass | 60,600 or 71,100 kg (133,600 or 156,700 lb) | 1.00 | infobox |
| Ares V | Maximum thrust | SL: 14.6 MN (3,280,000 lbf) | 1.00 | infobox |
| Ares V | Maximum thrust | vac: 16 MN (3,600,000 lbf) | 1.00 | infobox |
| Ares V | Maximum thrust | 5 × RS-68: 15,685 kN (3,526,000 lbf) | 1.00 | infobox |
| Ares V | Maximum thrust | 6 × RS-68: 18,822 kN (4,231,000 lbf) | 1.00 | infobox |
| Ares V | Maximum thrust | 5 × RS-25: 11,395 kN (2,562,000 lbf) | 1.00 | infobox |
| Ares V | No. boosters | 2 | 1.00 | infobox |
| Ares V | Powered by | 5 × RS-25 or | 1.00 | infobox |
| Ares V | Powered by | 5 × RS-68B or | 1.00 | infobox |
| Ares V | Powered by | 6 × RS-68B | 1.00 | infobox |
| Ares V | Powered by | 1 or 2 × J-2X | 1.00 | infobox |
| Ares V | Propellant | APCP (Al / AP / PBAN) | 1.00 | infobox |
| Ares V | Propellant | LH2 / LOX | 1.00 | infobox |
| Ares V | Specific impulse | 269 s (2.64 km/s) | 1.00 | infobox |
| Ares V | Stages | 2 | 1.00 | infobox |
| Ares V | Status | Canceled | 1.00 | infobox |
| Ares V | Total launches | 0 | 1.00 | infobox |
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