TDRS-1, known before launch as TDRS-A, was an American communications satellite, operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by TRW and launched by Space Shuttle Challenger on its maiden flight, STS-6.[3]
![]() TDRS-1 and its IUS aboard Challenger shortly before deployment. | |
Mission type | Communication |
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Operator | NASA |
COSPAR ID | 1983-026B ![]() |
SATCAT no. | 13969 [1] |
Mission duration | Planned: 10 years Final: 26 years, 6 months, 16 days |
Spacecraft properties | |
Bus | TDRS |
Manufacturer | TRW |
Launch mass | 2,268 kg (5,000 lb)[2] |
Dimensions | 17.4 × 12.9 m (57 × 42 ft)[2] |
Power | 1700 watts[2] |
Start of mission | |
Launch date | 4 April 1983, 18:30:00 (1983-04-04UTC18:30) UTC |
Rocket | Space Shuttle Challenger STS-6 / IUS |
Launch site | Kennedy Space Center, LC-39A |
Contractor | Rockwell International |
End of mission | |
Disposal | Retired to graveyard |
Declared | 21 October 2009 |
Deactivated | 27 June 2010 (2010-06-28) |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Epoch | 1 April 1984 [1] |
While on the pad, problems were detected with Challenger main engines and repairs were begun. During this time, a severe storm caused contamination of TDRS-1 while it was in the Payload Change-out Room on the Rotating Service Structure at the launch pad. Consequently, the satellite had to be taken back to its checkout facility, where it was cleaned and rechecked.[4] Challenger finally lifted off from Launch Complex 39A of the Kennedy Space Center at 18:30:00 UTC on 4 April 1983.[5]
Following deployment from Challenger, TDRS-1 was to be raised to its operational geosynchronous orbit by means of an Inertial Upper Stage, which consisted of two solid rocket motors, the first used to raise the orbit's apogee, the second its perigee. The first burn was successful, however the IUS went out of control during the second burn. TDRS-1 separated from the upper stage in a lower than planned orbit. It was eventually raised to geosynchronous orbit by means of its attitude control system.[6] In order to achieve this, a team of engineers from the Goddard Space Flight Center in Greenbelt, Maryland worked for nearly three months using six one-pound thrusters on the errant satellite to push it 8,600 miles (13,800 km) higher in space. The failure was later identified as a collapsed second-stage nozzle Techroll Seal, a flexible ring which allows the nozzle to move and provide directional control.[7] The Goddard engineers' successful effort required 39 adjustment burns to correct the elliptical orbit to the 22,300 mi (35,900 km) high geosynchronous orbit desired for TDRS-1. In connection with this rescue, Goddard Space Flight Center on 26 November 1984 honored a group of 34 individuals with the Robert H. Goddard Award of Merit, the highest level of recognition the Goddard Space Flight Center can bestow on its employees.[7] In 1989 its operations were affected by a geomagnetic storm.[8]
TDRS-1 formed part of the first Pole-to-Pole phone call on 28 April 1999, with TDRS-1 being used at the South Pole, and an Iridium phone being used at the North Pole (recorded in Ripley's Believe It Or Not and Guinness World Records in April 1999).[9]
TDRS-1 had a design life of ten years, however in April 2008, it was still operational on the twenty-fifth anniversary of its launch.[10] Over the years, the orbital inclination was allowed to increase so that, for portions of the day (approximately 5 hours), it was able to be used for communications with the North and then the South Pole. Along with Marisat F2, GOES 3 and LES-9, it was one of a number of satellites that were transferred to the US National Science Foundation in 1998,[11] for communications with the Amundsen–Scott South Pole Station.[12] After Marisat was retired, TDRS-1 became the primary means of communication with the research station.[12] The last functioning traveling-wave tube amplifier aboard TDRS-1 failed in October 2009,[11] rendering the spacecraft unusable for communications purposes.
TDRS-1 proved helpful during a 1999 medical emergency at the NSF's Antarctic Amundsen–Scott South Pole Station. The satellite's high-speed Internet connectivity allowed personnel to conduct telemedicine conferences. Doctors in the United States aided Dr. Jerri Nelson, who had breast cancer, in performing a self-biopsy and administering chemotherapy. Later, in 2002, doctors used TDRS-1 to perform another telemedicine conference with the station to assist in knee surgery for a meteorologist.[11]
Because of its orbit, the satellite was able to link the North and South Poles and relayed the first pole-to-pole phone call. TDRS-1 also transmitted the first internet connection and live webcast from the North Pole and supported the first global television event from the South Pole Station - a worldwide television broadcast to commemorate the beginning of the year 2000.[11]
The spacecraft was retired on or about 21 October 2009, after 26 years. Decommissioning was started on 5 June 2010 and passivation was completed on 27 June 2010.[13] As of 2009[update], NASA had repositioned TDRS-3 to assume the duties of TDRS-1.[14]
Tracking and Data Relay Satellite System | ||
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First generation | ||
Second generation | ||
Third generation | ||
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← 1982 · Orbital launches in 1983 · 1984 → | |
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Kosmos 1428 | Kosmos 1429 · Kosmos 1430 · Kosmos 1431 · Kosmos 1432 · Kosmos 1433 · Kosmos 1434 · Kosmos 1435 · Kosmos 1436 | Kosmos 1437 | Unnamed | IRAS · PIX-2 | Kosmos 1438 | Sakura 2a | Kosmos 1439 | OPS 0252 · OPS 0252 SSU-1 · OPS 0252 SSU-2 · OPS 0252 SSU-3 · LIPS-2 | Kosmos 1440 | Kosmos 1441 | Tenma | Kosmos 1442 | Kosmos 1443 | Kosmos 1444 | Molniya-3 No.34 | Ekran No.18L | Kosmos 1445 | Kosmos 1446 | Molniya-1-56 | Astron | Kosmos 1447 | NOAA-8 | Kosmos 1448 | Kosmos 1449 | Molniya-1 No.68 | STS-6 (TDRS-1) | Kosmos 1450 | Gran' No.23L | Kosmos 1451 | Satcom 1R | Kosmos 1452 | OPS 2925 | Rohini RS-D2 | Kosmos 1453 | Soyuz T-8 | Kosmos 1454 | Kosmos 1455 | Kosmos 1456 | Kosmos 1457 | Kosmos 1458 | GOES 6 | Kosmos 1459 | Kosmos 1460 | Kosmos 1461 | Kosmos 1462 | Kosmos 1463 | Intelsat V F-6 | Kosmos 1464 | Kosmos 1465 | Kosmos 1466 | EXOSAT | Kosmos 1467 | Venera 15 | Venera 16 | Kosmos 1468 | OPS 6432 · OPS 6432 SSU-1 · OPS 6432 SSU-2 · OPS 6432 SSU-3 | Kosmos 1469 | ECS-1 · OSCAR-10 | STS-7 (Anik C2 · Palapa B1 · SPAS-01 · OSTA-2) | OPS 0721 · OPS 3899 | Kosmos 1470 | Soyuz T-9 | HILAT | Kosmos 1471 | Galaxy 1 | Gorizont No.17L | Prognoz 9 | Kosmos 1472 | Kosmos 1473 · Kosmos 1474 · Kosmos 1475 · Kosmos 1476 · Kosmos 1477 · Kosmos 1478 · Kosmos 1479 · Kosmos 1480 | Kosmos 1481 | Kosmos 1482 | OPS 7994 | Molniya-1 No.66 | Kosmos 1483 | Kosmos 1484 | Kosmos 1485 | Telstar 301 | OPS 7304 | Kosmos 1486 | Kosmos 1487 | Sakura 2b | Kosmos 1488 | Kosmos 1489 | Kosmos 1490 · Kosmos 1491 · Kosmos 1492 | Progress 17 | Fanhui Shi Weixing 6 | Kosmos 1493 | Gran' No.24L | STS-8 (INSAT-1B) | Molniya-3 No.32 | Kosmos 1494 | Kosmos 1495 | Kosmos 1496 | Satcom 2R | Kosmos 1497 | Kosmos 1498 | Kosmos 1499 | Galaxy-2 | Soyuz 7K-ST No. 16L | Kosmos 1500 | Ekran No.25L | Kosmos 1501 | Kosmos 1502 | Kosmos 1503 | Kosmos 1504 | Intelsat V F-7 | Progress 18 | Kosmos 1505 | Kosmos 1506 | Meteor-2 No.10 | Kosmos 1507 | Kosmos 1508 | Kosmos 1509 | OPS 1294 | Molniya-1 No.48 | Kosmos 1510 | STS-9 | Kosmos 1511 | Gorizont No.18L | Kosmos 1512 | Kosmos 1513 | Kosmos 1514 | Kosmos 1515 | Molniya-3 No.35 | Kosmos 1516 | Kosmos 1517 | Kosmos 1518 | Kosmos 1519 · Kosmos 1520 · Kosmos 1521 | |
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). |