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The Polyot (Russian: Полёт, lit. 'flight', GRAU index: 11A59) was an interim orbital carrier rocket, built to test ASAT spacecraft. It was required as a stopgap after the cancellation of the UR-200 programme, but before the Tsyklon could enter service. Only two were ever launched, the first on 1 November 1963, and the last on 12 April 1964. Both of these…
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rocket r-7 orbital spacecraft asat ur-200 tsyklon polyot 11a59 first last boosters 400 100 lb 300 190 mi 59 family
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Polyot (rocket) | Altitude | 300 km (190 mi) | 1.00 | infobox |
| Polyot (rocket) | Burn time | 119 seconds | 1.00 | infobox |
| Polyot (rocket) | Burn time | 240 seconds | 1.00 | infobox |
| Polyot (rocket) | Country of origin | Soviet Union | 1.00 | infobox |
| Polyot (rocket) | Diameter | 2.99 m (9 ft 10 in) | 1.00 | infobox |
| Polyot (rocket) | Family | R-7 | 1.00 | infobox |
| Polyot (rocket) | First flight | 1 November 1963 | 1.00 | infobox |
| Polyot (rocket) | Function | Small-lift launch vehicle | 1.00 | infobox |
| Polyot (rocket) | Height | 30 m (98 ft) | 1.00 | infobox |
| Polyot (rocket) | Last flight | 12 April 1964 | 1.00 | infobox |
| Polyot (rocket) | Launch sites | Baikonur, Site 31/6 | 1.00 | infobox |
| Polyot (rocket) | Manufacturer | OKB-1 | 1.00 | infobox |
| Polyot (rocket) | Mass | 277,000 kg (611,000 lb) | 1.00 | infobox |
| Polyot (rocket) | Mass | 1,400 kg (3,100 lb) | 1.00 | infobox |
| Polyot (rocket) | Maximum thrust | 995.3 kN (223,800 lbf) | 1.00 | infobox |
| Polyot (rocket) | Maximum thrust | 294 kN (66,000 lbf) | 1.00 | infobox |
| Polyot (rocket) | No. boosters | 4 | 1.00 | infobox |
| Polyot (rocket) | Orbital inclination | 59° | 1.00 | infobox |
| Polyot (rocket) | Powered by | 1 × RD-107-8D74K | 1.00 | infobox |
| Polyot (rocket) | Powered by | 1 × RD-108 | 1.00 | infobox |
| Polyot (rocket) | Propellant | LOX / RP-1 | 1.00 | infobox |
| Polyot (rocket) | Specific impulse | 257 s (2.52 km/s) | 1.00 | infobox |
| Polyot (rocket) | Specific impulse | 330 s (3.2 km/s) | 1.00 | infobox |
| Polyot (rocket) | Stages | 1 | 1.00 | infobox |
| Polyot (rocket) | Status | Retired | 1.00 | infobox |
| Polyot (rocket) | Success(es) | 2 | 1.00 | infobox |
| Polyot (rocket) | Total launches | 2 | 1.00 | infobox |
| Polyot (rocket) | Total thrust | 3,981.2 kN (895,000 lbf) | 1.00 | infobox |
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