Kosmos 140 (Russian: Космос 140 meaning Cosmos 140), Soyuz 7K-OK No.3, was an uncrewed flight of the Soyuz spacecraft.[3] It was the third attempted test flight of the Soyuz 7K-OK model, after orbital (Kosmos 133) and launch (Soyuz 11A511) failures of the first two Soyuz spacecraft.
Mission type | Test flight |
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Operator | Experimental Design Bureau (OKB-1) |
COSPAR ID | 1967-009A ![]() |
SATCAT no. | 02667 |
Mission duration | 2 days |
Spacecraft properties | |
Spacecraft | Soyuz 7K-OK No.3 |
Spacecraft type | Soyuz 7K-OK |
Manufacturer | Experimental Design Bureau (OKB-1) |
Launch mass | 6450 kg[1] |
Landing mass | 2500 kg |
Dimensions | 7.13 m (23.4 ft) long 2.72 m (8 ft 11 in) wide |
Start of mission | |
Launch date | 7 February 1967, 03:21 GMT[2] |
Rocket | Soyuz 11A511 s/n U15000-03 |
Launch site | Baikonur, Site 1/5[1] |
Contractor | Experimental Design Bureau (OKB-1) |
End of mission | |
Landing date | 9 February 1967 |
Landing site | Aral Sea, Kazakhstan |
Orbital parameters | |
Reference system | Geocentric orbit[2] |
Regime | Low Earth orbit |
Perigee altitude | 165.0 km |
Apogee altitude | 218.0 km |
Inclination | 51.7° |
Period | 88.5 minutes |
Soyuz programme ← Soyuz 7K-OK No.1 |
The follow-up to Kosmos 133 (Soyuz 7K-OK No.2), 28 November 1966, was planned for 14 December 1966 (Soyuz 7K-OK No.1) but ended disastrously. At liftoff, the Blok A core stage of the 11A57 booster ignited, but not the strap-ons. A shutdown command was immediately sent and pad crews began to move the service towers back in place and drain the propellants. This task was completed for the core stage and strap-ons, and then about 27 minutes after the attempted launch, the launch escape system (LES) suddenly fired. Its exhaust caused the Blok I third stage propellant tanks to overheat and explode, killing one person on the ground and damaging the Soyuz and core stage/strap-ons beyond repair. LC-31 was also badly damaged and took seven months of repair work in the frigid Kazakhstan winter to be restored to use. The reason for the LES firing was thought to be either a timer being activated due to the Earth's rotation affecting the gyroscope package in the launch vehicle or perhaps one of the service towers bumping it.
In February 1967, the backup booster and spacecraft were set up at LC-1 and the planned mission could be carried out. Kosmos 140 was operated in a low Earth orbit, on 7 February 1967, it had a perigee of 165 km (103 mi), an apogee of 218 km (135 mi), an inclination of 51.7°, and an orbital period of 88.5 minutes.[2]
The spacecraft suffered attitude control problems and excessive fuel consumption in orbit, but remained controllable. An attempted maneuver on the 22nd orbit still showed problems with the control system. It malfunctioned yet again during retrofire, leading to a steeper than planned ballistic reentry and a 30 centimetres (12 in) hole being burned in the heat shield.[1]
Although the event would have been lethal to any human occupants, the capsule's recovery systems operated and the capsule crashed through the ice of the frozen Aral Sea, hundreds of kilometers short of its landing zone. The spacecraft finally sank in 10 metres of water and had to be retrieved by divers. The test performance was nonetheless deemed "good enough"; the crewed docking missions of Soyuz 1 and Soyuz 2 was approved for the next flight.
Soyuz programme | |||||||||||||||||||||||||||
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Main topics |
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Past missions (by spacecraft type) |
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Uncrewed missions are designated as Kosmos instead of Soyuz; exceptions are noted "(uncrewed)". The † sign designates failed missions. Italics designates cancelled missions. |
← 1966 · Orbital launches in 1967 · 1968 → | |
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Intelsat II F-2 | OPS 1664 | IDCSP 9 · IDCSP 10 · IDCSP 11 · IDCSP 12 · IDCSP 13 · IDCSP 14 · IDCSP 15 · IDCSP 16 | Kosmos 138 | Kosmos 139 | ESSA-4 | OV3-5 | OPS 4399 | Lunar Orbiter 3 | Kosmos 140 | OPS 6073 | Diadème 1 | Kosmos 141 | Kosmos 142 | Diadème 2 | OPS 4750 | OPS 4204 | Kosmos 143 | Kosmos 144 | Kosmos 145 | OSO 3 | Kosmos 146 | Kosmos 147 | Kosmos 148 | Kosmos 149 | Kosmos 150 · OGCh No.8 | Intelsat II F-3 | Kosmos 151 | Kosmos 152 | OPS 4779 | Kosmos 153 | ATS-2 · RPM-481 | Kosmos 154 | Kosmos 155 | Unnamed | OPS 0100 | Surveyor 3 | ESSA-5 | Soyuz 1 | San Marco 2 | OPS 4243 | Kosmos 156 | OPS 6638 · OPS 6679 · ERS-18 · ERS-20 · ERS-27 | Lunar Orbiter 4 | Ariel 3 | OPS 4696 · OPS 1967 | Kosmos 157 | Kosmos 158 | Kosmos 159 | Kosmos 160 | OPS 7218 | Kosmos 161 | OPS 4321 · OPS 5557 | Explorer 34 | Molniya-1 No.8 | ESRO-2A | NRL PL-151 · NRL PL-152 · NRL PL-153 · NRL PL-154 · NRL-PL 159 · Timation 1 · Calsphere 3 · Calsphere 4 · OPS 5712 | Kosmos 162 | OPS 4360 | Kosmos 163 | Kosmos 164 | Venera 4 | Kosmos 165 | Mariner 5 | Kosmos 166 | OPS 3559 · OPS 1873 | Kosmos 167 | Zenit-4 No.32 | OPS 4286 | Unnamed | SECOR-9 · Aurora | IDCSP 16 · IDCSP 17 · IDCSP 18 · IDCSP 19 · LES-5 · DODGE | Kosmos 168 | Surveyor 4 | Kosmos 169 | Explorer 35 | Zenit-4 No.33 | OPS 1879 | OV1-11 · OV1-12 · OV1-86 | OGO-4 | Kosmos 170 | Lunar Orbiter 5 | OPS 4827 | Kosmos 171 | Kosmos 172 | OPS 4886 | OPS 7202 | Kosmos 173 | Kosmos 174 | Zenit-2 No.51 | Biosatellite 2 | Surveyor 5 | Kosmos 175 | Kosmos 176 | OPS 5089 | Kosmos 177 | Kosmos 178 | OPS 4941 | Kosmos 179 | OPS 4947 | Kosmos 180 | Unnamed | 7K-L1 No.4L | Intelsat II F-4 | Molniya-1 No.9 | OPS 1264 | Kosmos 181 | Kosmos 182 | Kosmos 183 | OSO 4 | Molniya-1 No.12 | Kosmos 184 | OPS 4995 | Kosmos 185 | Kosmos 186 | Kosmos 187 | Kosmos 188 | Kosmos 189 | OPS 0562 · OPS 1587 | Kosmos 190 | ATS-3 | Surveyor 6 | Apollo 4 | ESSA-6 | Kosmos 191 | 7K-L1 No.5L | Kosmos 192 | Kosmos 193 | WRESAT | Kosmos 194 | OV3-6 | OPS 5000 | OPS 1001 | Pioneer 8 · ERS-30 | Kosmos 195 | Kosmos 196 | Kosmos 197 | Kosmos 198 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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