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Simorgh (Persian: ماهوارهبر سیمرغ, Simurgh), also called Safir-2, is an Iranian expendable launch vehicle. It is the successor of the Safir, Iran's first space launch vehicle. Its mission is to carry heavier satellites into higher orbit than Safir.
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launch safir first stage simorgh orbit 000 engines kn lbf iranian also thrust space vehicle rocket total seconds time saman-1
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Simorgh (rocket) | Burn time | 120 seconds | 1.00 | infobox |
| Simorgh (rocket) | Burn time | 320 seconds | 1.00 | infobox |
| Simorgh (rocket) | Burn time | 40 seconds | 1.00 | infobox |
| Simorgh (rocket) | Country of origin | Iran | 1.00 | infobox |
| Simorgh (rocket) | Diameter | 2.4 m (7 ft 10 in) first stage, 1.5 m (4 ft 11 in) second stage | 1.00 | infobox |
| Simorgh (rocket) | Diameter | 2.4 m | 1.00 | infobox |
| Simorgh (rocket) | Diameter | 1.5 m | 1.00 | infobox |
| Simorgh (rocket) | Failure | 3 or 4 | 1.00 | infobox |
| Simorgh (rocket) | Family | Derived from Safir | 1.00 | infobox |
| Simorgh (rocket) | First flight | 19 April 2016 (suborbital) 27 July 2017 (orbital) | 1.00 | infobox |
| Simorgh (rocket) | Function | Small-lift space launch vehicle | 1.00 | infobox |
| Simorgh (rocket) | Height | 25.9 m (85 ft) | 1.00 | infobox |
| Simorgh (rocket) | Height | 17.8 m | 1.00 | infobox |
| Simorgh (rocket) | Last flight | 6 December 2024 (orbital) | 1.00 | infobox |
| Simorgh (rocket) | Launch sites | Imam Khomeini Space Launch Terminal | 1.00 | infobox |
| Simorgh (rocket) | Mass | 87 t (192,000 lb) | 1.00 | infobox |
| Simorgh (rocket) | Mass | 800 kg (1,800 lb) | 1.00 | infobox |
| Simorgh (rocket) | Mass | 250 kg (550 lb) | 1.00 | infobox |
| Simorgh (rocket) | Mass | 400 kg (880 lb) | 1.00 | infobox |
| Simorgh (rocket) | Maximum thrust | 1,590 kN (360,000 lbf) | 1.00 | infobox |
| Simorgh (rocket) | Maximum thrust | 71.6 kN (16,100 lbf) | 1.00 | infobox |
| Simorgh (rocket) | Maximum thrust | 13 kN (2,900 lbf) | 1.00 | infobox |
| Simorgh (rocket) | Powered by | 4 × modified Shahab-3 engines + 4 verniers | 1.00 | infobox |
| Simorgh (rocket) | Powered by | 4 × LRE-4 (R-27 Zyb vernier engines) | 1.00 | infobox |
| Simorgh (rocket) | Powered by | Saman-1 | 1.00 | infobox |
| Simorgh (rocket) | Propellant | .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l… | 1.00 | infobox |
| Simorgh (rocket) | Propellant | N2O4 / UDMH | 1.00 | infobox |
| Simorgh (rocket) | Propellant | Solid | 1.00 | infobox |
| Simorgh (rocket) | Stages | 2 (optional 3rd stage) | 1.00 | infobox |
| Simorgh (rocket) | Status | Active | 1.00 | infobox |
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