| Lewis | |
| Mission Type: | Technology Remote sensing UV Astronomy |
| Operator: | NASA |
| Cospar Id: | 1997-044A |
| Mission Duration: | 1-3 years (planned) 3 days (achieved) |
| Spacecraft Bus: | T200B |
| Manufacturer: | TRW |
| Instruments: | HSI LEISA UCB |
| Launch Date: | UTC |
| Launch Rocket: | LMLV-1 (Athena I) |
| Launch Site: | Vandenberg SLC-6 |
| Launch Contractor: | Lockheed Martin |
| Decay Date: | 28 September 1997 |
| Orbit Epoch: | 23 August 1997, 02:51:01 UTC[1] |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Low Earth |
| Orbit Periapsis: | 124km (77miles) Planned: |
| Orbit Apoapsis: | 134km (83miles) Planned: |
| Orbit Inclination: | 97.5 degrees |
| Apsis: | gee |
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.
Lewis was a 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, a perigee of, and 97.5 degrees of inclination. Lewis was to have raised itself into a higher orbit, at an altitude of .[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]