STEX
Science Technology Experiments
STEX during ground-testing |
Names |
STEX USA 140 NROL-8 |
---|
|
Mission type |
Technology demonstration |
---|
Operator |
NRO |
---|
COSPAR ID |
1998-055A |
---|
SATCAT № |
25489 |
---|
|
Spacecraft properties |
---|
Manufacturer |
Lockheed Martin |
---|
Launch mass |
539.4 kg (1,189 lb) |
---|
|
Start of mission |
---|
Launch date |
10:04:49, October 3, 1998 (1998-10-03T10:04:49) |
---|
Rocket |
Taurus (rocket) |
---|
Launch site |
Vandenberg AFB |
---|
Space Technology Experiments, or STEX, also known as NRO Launch 8 or NROL-8, was an experimental NRO satellite built by Lockheed Martin. It was launched on October 3, 1998.[1] One of the experiments was ATEx (Advanced Tether Experiment), which was deployed on 22. January 1999, and subsequently jettisoned.[2]
ATEx
Advanced Tether Experiment (ATEx) with partially deployed upper end-body
The Advanced Tether Experiment (ATEx), was a follow on to the TiPS experiment, designed and built by the Naval Center for Space Technology, flown as one of the experiments on STEX. ATEx had two end masses connected by a polyethylene tether that was intended to deploy to a length of 6 km in length, and was intended to test a new space tether deployment scheme, new tether material, active control, and survivability. ATEx was deployed on 16 January 1999 and ended 18 minutes later after deploying only 22 m of tether. The jettison was triggered by an automatic protection system designed to save STEX if the tether began to stray from its expected departure angle,[3] which was ultimately caused by excessive slack tether,[4] As a result of the deployment failure, none of the desired ATEx goals were achieved.[5] ATEX is now tracked as a separate object as USA 141 or COSPAR ID 1998-055C.[6]
References
- ↑ "STEX". NSSDC Master Catalog Search. 2010-10-08.
- ↑ "ATEx". NSSDC Master Catalog Search. 2010-10-08.
- ↑ U. S. Naval Research Laboratory, Advanced Tether Experiment (ATEx) (retrieved 8 June 2016).
- ↑ Stephen S. Gates, Stephen M. Koss, and Michael F. Zedd, "Advanced Tether Experiment Deployment Failure," paper 99-413 presented at the American Astronautical Society/AIAA Astrodynamics Specialist Conference, Girdwood, AK, 16–19 August 1999; published in J. Spacecraft and Rockets, Vol. 38, No. 1, January– February 2001, pp. 60-68.
- ↑ Herbert J. Kramer, STEX (Space Technology Experiment) / ATEx, eoPortal, European Space Agency (retrieved 8 June 2016).
- ↑ "NSSDCA - STEX - Details". nssdc.gsfc.nasa.gov. NASA. Retrieved 23 June 2016.
External links
- STEX at Gunter's Space Page
|
---|
|
Imaging | |
---|
|
SIGINT | Radar location | |
---|
| Ship location | |
---|
| ELINT | |
---|
|
---|
|
Communication | |
---|
|
Technology | |
---|
|
---|
|
Lunar Prospector | Skynet 4D | Ofek-4 | STS-89 | Soyuz TM-27 | USA-137 | Brasilsat B3 · Inmarsat-3 F5 | Orbcomm FM3 · Orbcomm FM4 · GFO · Ad Astra | Globalstar 1 · Globalstar 2 · Globalstar 3 · Globalstar 4 | Kosmos 2349 | Iridium 50 · Iridium 52 · Iridium 53 · Iridium 54 · Iridium 56 | Kakehashi | SNOE · Teledesic 1 | Hot Bird 4 | Intelsat 806 | Progress M-38 (VDU-2) | USA-138 | SPOT 4 | Iridium 51 · Iridium 61 | Iridium 55 · Iridium 57 · Iridium 58 · Iridium 59 · Iridium 60 | TRACE | Iridium 62 · Iridium 63 · Iridium 64 · Iridium 65 · Iridium 66 · Iridium 67 · Iridium 68 | STS-90 | Globalstar 6 · Globalstar 8 · Globalstar 14 · Globalstar 15 | Nilesat 101 · BSat-1B | Kosmos 2350 | Iridium 69 · Iridium 71 | Kosmos 2351 | EchoStar IV | USA-139 | NOAA-15 | Progress M-39 | Iridium 70 · Iridium 72 · Iridium 73 · Iridium 74 · Iridium 75 | Zhongwei 1 | STS-91 | Thor 3 | Kosmos 2352 · Kosmos 2353 · Kosmos 2354 · Kosmos 2355 · Kosmos 2356 · Kosmos 2357 | Intelsat 805 | Kosmos 2358 | Kosmos 2359 | Molniya 3-49 | Nozomi | Shtil-1 · Tubsat-N · Tubsat-N1 | Resurs-O1 #4 · Fasat-Bravo · TMSAT · Gurwin Techsat 1B · WESTPAC · SAFIR-2 | Sinosat-1 | Kosmos 2360 | Orbcomm FM13 · Orbcomm FM14 · Orbcomm FM15 · Orbcomm FM16 · Orbcomm FM17 · Orbcomm FM18 · Orbcomm FM19 · Orbcomm FM20 | Mercury 3 | Soyuz TM-28 | Iridium 3 · Iridium 76 | ST-1 | Galaxy 10 | Astra 2A | Kwangmyŏngsŏng-1 | Iridium 77 · Iridium 79 · Iridium 80 · Iridium 81 · Iridium 82 | Globalstar 5 · Globalstar 7 · Globalstar 9 · Globalstar 10 · Globalstar 11 · Globalstar 12 · Globalstar 13 · Globalstar 16 · Globalstar 17 · Globalstar 18 · Globalstar 20 · Globalstar 21 | PAS-7 | Orbcomm FM21 · Orbcomm FM22 · Orbcomm FM23 · Orbcomm FM24 · Orbcomm FM25 · Orbcomm FM26 · Orbcomm FM27 · Orbcomm FM28 | Molniya-1T #99 | STEX (USA-141) | Eutelsat W2 · Sirius 3 | Hot Bird 5 | USA-140 | Maqsat 3 | Deep Space 1 · SEDSAT-1 | Progress M-40 ( Sputnik 41) | AfriStar · GE-5 | STS-95 (SPARTAN-201 · PANSAT) | PAS-8 | Iridium 2 · Iridium 83 · Iridium 84 · Iridium 85 · Iridium 86 | Zarya / ISS | Bonum 1 | STS-88 ( Unity · PMA-1 · PMA-2 · SAC-A · MightySat-1 | Satmex 5 | SWAS | Nadezhda 5 · Astrid 2 | Mars Climate Orbiter | Iridium 11 · Iridium 20 | PAS-6B | Kosmos 2361 | Kosmos 2362 · Kosmos 2363 · Kosmos 2364 |
|
Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |