3 stage vehicle consisting of 2 x MLRS + 1 x SR19 + 1 x SR19

Manufacturer: OSC. Launches: 5. First Launch Date: 1999-09-06. Last Launch Date: 2006-04-28. Launch data is: continuing. Apogee: 300 km (180 mi). Liftoff Thrust: 267.000 kN (60,023 lbf). Total Mass: 15,000 kg (33,000 lb). Core Diameter: 1.32 m (4.33 ft). Total Length: 15.50 m (50.80 ft).

1999 September 6 - Launch Site: Wake Island. Launch Vehicle: SR19/SR19.

• TCMP-3A re-entry vehicle test flight Nation: USA. Agency: OSC. Apogee: 300 km (180 mi). References: 1108.

• TCMP-3B Sensors mission Nation: USA. Agency: USA SSDC. Apogee: 300 km (180 mi). References: 1108.

• PAC-3 OT-2a Target mission Nation: USA. Agency: USA SSDC. Apogee: 270 km (160 mi). References: 1812.

• CMCM-1 Target mission Nation: USA. Agency: MDA. Manufacturer: MIT/LL. Apogee: 200 km (120 mi). A two-stage SR19 rocket was flown from the Kaui Test Facility in the Pacific Missile Range Facility. The payload included the deployment of complex countermeasures, a mock reentry vehicle, an onboard sensor package. This series of radar certification flight was initially part of the Block 2004 effort.

• CMCM-2 Target mission Nation: USA. Agency: MDA. Manufacturer: MIT/LL. Apogee: 200 km (120 mi). This countermeasures test was a repeat of the one held on April 13, 2006. MDA tested its radars in the Pacific Missile Test Facility in Hawaii against a target missile that carried countermeasures, a mock warhead, and an onboard sensor package. No interceptor missiles were used.

• McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.