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Indonesian National Institute of Aeronautics and Space's solid fuel rockets are classified as "RX" (''Roket Eksperimental''), followed by their diameter in millimeters. For example, the RX-100 has a diameter of 100 mm.〔http://indomil.wordpress.com/2009/05/24/lapan-and-indonesian-rocket-program/〕 ==Rocket engines== This family is composed by:〔http://www.b14643.de/Spacerockets_1/Rest_World/RPS-01/Description/Frame.htm〕 *RX-75 *RX-100 (Diameter of 110 mm length of 1900 mm mass of 30 kg and length of 1900 mm. Functions: to test rocket payload subsystems. Propellant type: solid-composite Fuel time: 2.5 seconds, Flight time: 70 seconds Maximum speed: Mach 1. Range: 11 km, 7000m altitude, Payload: Diagnostic,: GPS, altitude meter, gyro, 3-axis accelerometer, CPU processor and battery.) *RX-150 *RX-250 (part of RX-250-LPN) (Gross mass 300 kg, height 5.30 m, diameter 0.25 m, thrust 52.00 kN, burn time 6.00 s. Eight launches from 1987 to 2007.〔http://www.astronautix.com/lvs/rx250.htm〕〔http://www.astronautix.com/mfrs/lapan.htm〕) *RX-320 (part of Pengorbitan-2) (Thrust 52.00 kN, burn time 9.00 s.〔http://www.b14643.de/Spacerockets_1/Rest_World/RPS-01/Description/Frame.htm〕 Launched on 2 July and 30 May 2008 from Pameungpeuk, West Java〔http://www.astronautix.com/mfrs/lapan.htm〕) *RX-420 (part of Pengorbitan-1) (Thrust 94.10 kN, burn time 12.30 s.〔http://www.b14643.de/Spacerockets_1/Rest_World/RPS-01/Description/Frame.htm〕 Launched on 2 July 2009 from Pameungpeuk, West Java〔http://www.astronautix.com/mfrs/lapan.htm〕 ) *RX-550 (part of Pengorbitan-2) (Thrust 245.20 kN, burn time 15.00 s.〔http://www.b14643.de/Spacerockets_1/Rest_World/RPS-01/Description/Frame.htm〕 Planned〔(【引用サイトリンク】title=LAPAN prepares rocket launch in Morotai (Indonesian) )〕) *RX-750 (planned) *RX-980 (date mars=June 4, 1997) 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「RX (rocket family)」の詳細全文を読む スポンサード リンク
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