Kosmos 1402 (Russian: Космос 1402) was a Soviet spy satellite that malfunctioned, resulting in the uncontrolled re-entry of its nuclear reactor and its radioactive uranium fuel. Kosmos 1402 was launched on August 30, 1982, and re-entered the atmosphere on 23 January 1983. The fission reactor entered a few days later; on 7 February 1983.
Mission type | Ocean reconnaissance |
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COSPAR ID | 1982-084A ![]() |
SATCAT no. | 13441 |
Spacecraft properties | |
Spacecraft type | US-A |
BOL mass | 3,000 pounds (1,400 kg) |
Power | 2 kW BES-5 fission reactor |
Start of mission | |
Launch date | 30 August 1982, 10:06 (1982-08-30UTC10:06Z) UTC[1] |
Rocket | Tsyklon-2 |
Launch site | Tyuratam missile and space complex (now Baikonur launchpad 90) |
End of mission | |
Disposal | Decommissioned |
Decay date | 23 January 1983 Reactor: 7 February 1983 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.00188 |
Perigee altitude | 251 kilometres (156 mi) |
Apogee altitude | 263 kilometres (163 mi) |
Inclination | 65.6 degrees |
Period | 89.64 minutes |
Epoch | 29 September 1982[2] |
Kosmos 1402 was a RORSAT surveillance satellite that used radar for monitoring NATO vessels. The power source for the satellite was a BES-5 nuclear fission reactor, which used about 50 kilograms (110 lb) of enriched uranium as a fuel source. The satellite operated in low Earth orbit, and the reactor was designed to eject to a higher parking orbit at the end of the satellite's mission, or in the event of a mishap. This ejection mechanism was implemented in the RORSAT satellites after a nuclear accident caused by a previous malfunction of Kosmos 954, five years earlier over Canada's Northwest Territories.[3]
In response to the Kosmos 954 mishap, RORSAT satellites were modified with an ejection system for their nuclear reactors. This ejections system would allow the reactor section to be ejected in the event of a malfunction, or at the end of the satellite's service life, so the radioactive core could be placed in a disposal orbit (about 1000 km), where the fuel would remain for 500 years.[4]
On 28 December 1982, the ejection system in Kosmos 1402 failed to adequately jettison the reactor to a higher orbit, and the satellite split into three parts and began to tumble out of control.[5] The three main sub-components were the reactor with its booster engine, the instrument section of the satellite with the expended second stage of the launch vehicle, and the radar antenna.[4]
If the uranium core were to explode or shatter in the atmosphere, and radioactive fragments fell near a populated area, the resulting nuclear contamination could have caused a significant and widespread hazard.[5][6] Because of this concern, the soviet engineers had re-designed the reactor to completely burn up in the atmosphere, so that nothing would reach the ground. But this information was not verified by other countries at the time.[7][8]
The uncertainty of the reentry location and time, coupled with concerns of radioactive contamination, triggered many countries to place emergency response teams on high alert. Military aircraft, ships, and personnel were mobilized in anticipation. Countries with response plans included United States, Canada, Belgium, Australia,[6] Oman, UAE, West Germany, France and Sweden.[9]
The antenna section was the first part of the satellite to re-enter, it burned up in the atmosphere on December 30, 1982.
The main satellite bus of Kosmos 1402 reentered the Earth's atmosphere on January 23, 1983, south of Diego Garcia in the Indian Ocean (25°S 84°E). No debris was recovered, but it is believed that the satellite disintegrated then crashed into the sea. The satellite was visible over the United Kingdom, for about a minute, on the night before impact.[9]
The reactor section and core continued to orbit for another two weeks, it re-entered on February 7, 1983, over the South Atlantic Ocean, near Ascension Island (19°S 22°W). The reactor is believed to have completely burned up into particles and dispersed to safe levels of atmospheric radioactivity.
Subsequent RORSATs were equipped with a backup (secondary) core ejection mechanism – when the primary ejection mechanism failed on Kosmos 1900 in 1988 this system succeeded in raising the core to a safe disposal orbit.[10] After this accident, launches of new US-A series satellites were stopped for a year and a half.
Radioactive strontium was detected in rain samples from Fayetteville, Arkansas in the months following the incident. The radioactive material originated in the Kosmos 1402 core.[11] Another investigation determined that 44 kg of uranium had been dispersed into the stratosphere after the incident.[12]
The incident triggered widespread discussion about nuclear technology in space, including topics related to space law, insurance and liability, militarization, nuclear safety, and security.
← 1981 · Orbital launches in 1982 · 1983 → | |
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Kosmos 1331 | Kosmos 1332 | Kosmos 1333 | Satcom 4 | Kosmos 1334 | OPS 2849 | Kosmos 1335 | Kosmos 1336 |Ekran No.22L | Kosmos 1337 | Kosmos 1338 | Kosmos 1339 | Kosmos 1340 |Westar 4 | Molniya 1-53 | Kosmos 1341 | Taifun-2 | Intelsat V F-4 | Kosmos 1342 | OPS 8701 | Gorizont No.14L | Kosmos 1343 | STS-3 | Molniya 3-18 | Kosmos 1344 | Meteor 2-8 | Kosmos 1345 | Kosmos 1346 | Kosmos 1347 | Kosmos 1348 | Kosmos 1349 | INSAT-1A | Kosmos 1350 | Salyut 7 (Iskra 2) | Kosmos 1351 |Kosmos 1352 | Kosmos 1353 | Kosmos 1354 | Kosmos 1355 | Kosmos 1356 | Kosmos 1357 · Kosmos 1358 · Kosmos 1359 · Kosmos 1360 · Kosmos 1361 · Kosmos 1362 · Kosmos 1363 · Kosmos 1364 | OPS 5642 · OPS 6553 | Soyuz T-5 | Kosmos 1365 | Zenit-6 | Kosmos 1366 | Kosmos 1367 | Kosmos 1368 | Progress 13 | Kosmos 1369 | Kosmos 1370 | Molniya 1-54 | Kosmos 1371 | Kosmos 1372 | Kosmos 1373 | Kosmos 1374 | Kosmos 1375 | Kosmos 1376 | Kosmos 1377 | Westar 5 | Kosmos 1378 | Yantar-4K2 | Kosmos 1379 | Kosmos 1380 | Kosmos 1381 | Soyuz T-6 | Kosmos 1382 | STS-4 | Kosmos 1383 | Kosmos 1384 | Kosmos 1385 | Kosmos 1386 | Progress 14 | Kosmos 1387 | Landsat 4 | Kosmos 1388 · Kosmos 1389 · Kosmos 1390 · Kosmos 1391 · Kosmos 1392 · Kosmos 1393 · Kosmos 1394 · Kosmos 1395 | Molniya 1-55 | Ekran No.23L | Kosmos 1396 | Kosmos 1397 | Kosmos 1398 | Kosmos 1399 | Kosmos 1400 | Soyuz T-7 | Kosmos 401 | Anik D1 | Molniya 3-19 | Kosmos 1402 | Strela-2M | Kosmos 1403 | Kosmos 1404 | Kiku-4 | Kosmos 1405 | Kosmos 1406 | Marecs B · Sirio 2 | Fanhui Shi Weixing 0-5 | Kosmos 1407 | Kosmos 1408 | Ekran No.24L | Progress 15 (Astrozond) | Kosmos 1409 | Kosmos 1410 | Intelsat V F-5 | Kosmos 1411 | Kosmos 1412 | Kosmos 1413 · Kosmos 1414 · Kosmos 1415 | Kosmos 1416 | Kosmos 1417 | Gorizont No.16L | Kosmos 1418 | Satcom 5 | DSCS II F-16 · DSCS III A-1 | Progress 16 (Iskra 3) | Kosmos 1419 | Kosmos 1420 | STS-5 (SBS-3 · Anik C3) | OPS 9627 | Kosmos 1421 | Strela-1M (x8) | Gran' No.21L | Kosmos 1422 | Kosmos 1423 | Meteor 2-9 | Kosmos 1424 | OPS 9845 | Kosmos 1425 | Gran' No.22L | Kosmos 1426 | Kosmos 1427 | |
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). |
Nuclear-powered Earth satellites | |
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Examples |
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Re-entered |
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See also Category:Nuclear power in space |