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Rubin
Rubin-3-DSI
Rubin-3-DSI
Credit: Manufacturer Image
German technology microsatellite. Rubin was developed by OHB and students of the Hochschule Bremen. Technology satellite for OHB-System, Germany. Launched 2000. Used the Kosmos-3M second stage bus.

Status: Operational 2000. First Launch: 2000-07-15. Last Launch: 2009-09-23. Number: 8 . Gross mass: 37 kg (81 lb).


More at: Rubin.

Subtopics

Rubin 3-DSI, 4-DSI Technology satellite for OHB-System, Germany. Launched 2002-2003. Used the Kosmos-3M second stage bus.

Rubin 2 (AATiS-OSCAR 49, AO 49) Technology satellite for OHB-System, Germany. Launched 2002.

Rubin 5-ASOLANT Technology satellite for OHB-System, Germany. Launched 2005. Used the Kosmos-3M second stage bus.

Rubin 7-AIS Technology satellite for OHB-System, Germany. Launched 2007. Used the Kosmos-3M second stage bus.

Rubin 8-AIS Technology satellite for OHB-System, Germany. Launched 2008.

Rubin 9 Technology satellite for LuxSpace (#9.1), OHB-System (#9.2), Germany, Luxembourg. Launched 2009.

Family: Communications, Technology, Technology satellite. Country: Germany. Launch Vehicles: R-14, Kosmos 3, Kosmos 11K65M, PSLV, Dnepr. Launch Sites: Baikonur, Plesetsk, Plesetsk LC132/1, Sriharikota, Baikonur LC109. Agency: RVSN, Bremen. Bibliography: 2, 552, 554.
Photo Gallery

Rubin-8-AISRubin-8-AIS
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RubinRubin
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Rubin 2Rubin 2
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Rubin-9.2Rubin-9.2
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Rubin-8-AISRubin-8-AIS
Credit: Manufacturer Image


Rubin-5Rubin-5
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2000 July 15 - . 12:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Rubin - . Nation: Germany. Agency: RVSN. Manufacturer: Bremen. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rubin. Decay Date: 2001-08-30 . USAF Sat Cat: 26406 . COSPAR: 2000-039C. Apogee: 463 km (288 mi). Perigee: 411 km (255 mi). Inclination: 87.2558 deg. Period: 93.23 min. Rubin was a microsatellite to measure launch vehicle parameters developed by OHB and students of the Hochschule Bremen. Rubin remained attached to the payload adapter of the Kosmos-3M final stage..

2002 November 28 - . 06:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Rubin-3-DSI - . Mass: 80 kg (176 lb). Nation: Russia. Agency: NCST. Manufacturer: AKO Polyot, Bremen. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rubin. USAF Sat Cat: 27561 . COSPAR: 2002-054C. Apogee: 748 km (464 mi). Perigee: 687 km (426 mi). Inclination: 98.2000 deg. Period: 99.10 min.

    Delayed from September 12, October 29. Rubin-3-DSI, with a mass of 45 kg, was built by PO Polyot of Omsk (builders of the Kosmos-3M) and OHB System of Bremen. It remained attached to the booster final stage and measured the launch vehicle environment and performance


2002 December 20 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Rubin 2 - . Mass: 45 kg (99 lb). Nation: Germany. Agency: Makeyev bureau. Manufacturer: Bremen. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 27609 . COSPAR: 2002-058E. Apogee: 645 km (400 mi). Perigee: 639 km (397 mi). Inclination: 64.6000 deg. Period: 97.60 min. Messaging technology satellite..

2003 September 27 - . 06:12 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Rubin 4-DSI - . Mass: 45 kg (99 lb). Nation: Germany. Agency: KVR. Class: Technology. Type: Communications technology satellite. Spacecraft: Rubin. USAF Sat Cat: 27945 . COSPAR: 2003-042G. Apogee: 693 km (430 mi). Perigee: 676 km (420 mi). Inclination: 98.2000 deg. Period: 98.50 min.

    RUBIN-4-dsi remained attached to the Kosmos launch vehicle final stage. The orbital telematics experiment transmited information on the rocketís acceleration, vibration load and position via e-mail using the Orbcomm satellite communications system. In this way, it will be possible to track the rocket in orbit reliably and without any data loss. RUBIN-4-dsi was the fourth micro-satellite from the RUBIN series developed and maintained by OHB.


2005 October 27 - . 06:52 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • Rubin-5 - . Mass: 45 kg (99 lb). Nation: Russia. Agency: KVR. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 28898 . COSPAR: 2005-043G. Apogee: 712 km (442 mi). Perigee: 684 km (425 mi). Inclination: 98.2000 deg. Period: 98.70 min. Technology/communications payload attached to the Kosmos 3M's upper stage It used the Orbcomm satellite system to return data to earth. Rubin-5 included the AATiS SAFIR-S amateur transponder and the ESA ASOLANT solar-powered GPS antenna experiment..

2008 April 28 - . 03:53 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
  • Rubin-8-AIS - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 32792 . COSPAR: 2008-021K. Apogee: 662 km (411 mi). Perigee: 619 km (384 mi). Inclination: 97.9000 deg. Period: 97.50 min. Remained attached to PSLV final stage; carried a payload for relaying identification beacon data from shipping..

2009 September 23 - . 06:21 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
  • Rubin-9.1 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.3000 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..
  • Rubin-9.2 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.3000 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..


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