Lewis was an American satellite which was to have been operated by NASA as part of the Small Satellite Technology Initiative. It carried two experimental Earth imaging instruments, and an ultraviolet astronomy payload. Due to a design flaw it failed within three days of reaching orbit, before it became operational.
Mission type | Technology Remote sensing UV Astronomy |
---|---|
Operator | NASA |
COSPAR ID | 1997-044A ![]() |
SATCAT no. | 24909![]() |
Mission duration | 1-3 years (planned) 3 days (achieved) |
Spacecraft properties | |
Bus | T200B |
Manufacturer | TRW |
Launch mass | 288 kilograms (635 lb) |
Start of mission | |
Launch date | 23 August 1997, 06:51:01 (1997-08-23UTC06:51:01Z) UTC |
Rocket | LMLV-1 (Athena I) |
Launch site | Vandenberg SLC-6 |
Contractor | Lockheed Martin |
End of mission | |
Last contact | 26 August 1997 (1997-08-27) |
Decay date | 28 September 1997 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 124 kilometers (77 mi) Planned: 523 kilometres (325 mi) |
Apogee altitude | 134 kilometers (83 mi) Planned: 523 kilometres (325 mi) |
Inclination | 97.5 degrees |
Epoch | 23 August 1997, 02:51:01 UTC[1] |
Instruments | |
HSI LEISA UCB | |
Lewis was a 288 kilograms (635 lb) spacecraft, which was designed to operate for between one and three years.[2] It was built by TRW under a contract which was signed on 11 July 1994.[2] Its primary instruments were the Hyperspectral Imager, the Linear Etalon Imaging Spectral Array and the Ultraviolet Cosmic Background experiment.[3] A number of technology demonstration payloads were also flown.
Lewis was launched by a LMLV-1 (Athena I) rocket flying from Space Launch Complex 6 at the Vandenberg Air Force Base.[4] The launch was originally scheduled to take place in September 1996, but it was delayed due to technical problems affecting the rocket.[5] Launch finally occurred at 06:51:01 GMT on 23 August 1997, and Lewis was successfully placed into a parking orbit with an apogee of 134 kilometres (83 mi), a perigee of 124 kilometres (77 mi), and 97.5 degrees of inclination. Lewis was to have raised itself into a higher orbit, at an altitude of 523 kilometres (325 mi).[3]
On 26 August, the satellite began spinning out of control at a rate of 2 rpm, which led to a loss of communications with ground controllers, and affected the ability of its solar arrays to generate power.[6] Controllers were unable to regain contact with the spacecraft,[7] and it was declared a total loss. It reentered the atmosphere at 11:58 GMT on 28 September 1997.[8] The cause of the failure was later established to be a design flaw in the spacecraft's attitude control system, which had been designed for the TOMS-EP spacecraft and was not sufficiently modified to be compatible with Lewis.[9]
← 1996 · Orbital launches in 1997 · 1998 → | |
---|---|
STS-81 | GPS IIR-1 | GE 2 · Nahuel 1A | Soyuz TM-25 | STS-82 | Haruka | Kosmos 2337 · Kosmos 2338 · Kosmos 2339 · Gonets-D1 #4 · Gonets-D1 #5 · Gonets-D1 #6 | JCSAT-R | USA-130 | Intelsat 801 | Mozhayets 2 | Tempo-2 | STS-83 | USA-131 | Progress M-34 | Kosmos 2340 | Thaicom 3 · BSAT-1a | Kosmos 2341 | Minisat 01 · Founders | GOES 10 | Iridium 4 · Iridium 5 · Iridium 6 · Iridium 7 · Iridium 8 | Chinasat 6A | Kosmos 2342 | STS-84 | Kosmos 2343 | Tselina-2 | Thor 2 | Telstar 5 | Inmarsat-3 F4 · INSAT-2D | Kosmos 2344 | Feng Yun 2A | Iridium 9 · Iridium 10 · Iridium 11 · Iridium 12 · Iridium 13 · Iridium 14 · Iridium 16 | Intelsat 802 | STS-94 | Progress M-35 | Iridium 15 · Iridium 17 · Iridium 18 · Iridium 20 · Iridium 21 | USA-132 | Superbird-C | OrbView-2 | Soyuz TM-26 | STS-85 (CRISTA-SPAS) | PAS-6 | Kosmos 2345 | Agila 2 | Iridium 22 · Iridium 23 · Iridium 24 · Iridium 25 · Iridium 26 | Lewis | ACE | PAS-5 | FORTE | Iridium MFS-1 · Iridium MFS-2 | Hot Bird 3 · Meteosat 7 | GE-3 | Iridium 27 · Iridium 28 · Iridium 29 · Iridium 30 · Iridium 31 · Iridium 32 · Iridium 33 | Kosmos 2346 · FAISAT-2V | Intelsat 803 | Molniya-1T #98 | STS-86 | Iridium 19 · Iridium 34 · Iridium 35 · Iridium 36 · Iridium 37 | IRS-1D | Progress M-36 (Sputnik 40 · X-Mir) | EchoStar III | Foton #11 | Cassini (Huygens) | Apstar 2R | USA-133 | STEP-4 | USA-135 · FalconGOLD | Maqsat-B · Maqsat-H · YES | SCD-2A | USA-134 | USA-136 | Iridium 38 · Iridium 39 · Iridium 40 · Iridium 41 · Iridium 43 | Kupon | Sirius 2 · IndoStar-1 | Resurs-F1M #1 | STS-87 (SPARTAN-201) | TRMM · Orihime · Hikoboshi | JCSAT-1B · Equator-S | Astra 1G | Iridium 42 · Iridium 44 | Galaxy 8i | Kosmos 2347 | Kosmos 2348 | Progress M-37 | Iridium 45 · Iridium 46 · Iridium 47 · Iridium 48 · Iridium 49 | Intelsat 804 | Orbcomm FM5 · Orbcomm FM6 · Orbcomm FM7 · Orbcomm FM8 · Orbcomm FM9 · Orbcomm FM10 · Orbcomm FM11 · Orbcomm FM12 | Early Bird 1 | AsiaSat 3 | |
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. |