| RME |
home
topic index |
|
Other Designations: Relay Mirror Experiment. Class: Military. Type: SDI. Nation: USA. Agency: SDIO. Manufacturer: Ball. The Relay Mirror Experiment (RME) was launched as a dual payload with LACE. Both satellites carried defense experiments intended to aid in design of space-based anti-missile lasers. RME validated stabilization, tracking, and pointing technologies at performance levels required for Strategic Defense Initiative (SDI) missions through a credible demonstration of a space-based relay mirror system. RME's 24-inch mirror was used to test laser pointing technology by deflecting ground-based beams back to earth. RME's attitude control system malfunctioned immediately after launch, shutting off a reaction wheel. Nevertheless the Maui Optical Observatory atop Mount Haleakala established the first relay on 26 June 1991, with Kihei, Hawaii. The precision relay mirror was 24 in. (61 cm) and had a pointing accuracy of 0.2 arcsec. The payload also included the Wideband Angular Vibration Experiment (WAVE), which measured low-level angular vibrations affecting performance of acquisition, tracking, and pointing (ATP) systems. Design Life: 6 months. Typical orbit: 457x478 km, include.=43.1 deg. Mass: 1,040 kg (2,290 lb). RME Chronology
Bibliography:
Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |