Satrec (original) (raw)

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

Satrec

Razaksat
Credit: Manufacturer Image

The South Korean Satrec Initiative built on earlier Kitsat technology to develop 100-kg and 200-kg satellite buses for national and international customers.

AKA: Razaksat. Status: Operational 2009. First Launch: 2009-07-14. Last Launch: 2009-07-29. Number: 2 .

Satrec Initiative provided two space buses:

The SI-100 100 kg platform was a flexible system for relatively small sized payloads. It was designed to satisfy the mission requirements by incorporating three-axis stabilized, accurate and agile attitude control. Dual redundancies were adapted where necessary in the system architecture design to increase the reliability of the satellite system.

The SI-100 platform, 0.65 m in width, 0.6 m in length and 0.85 m in height, had volume and mass suitable for piggy-back satellite launchers. For fixed solar panels, a 1 or 2 deployable panel configuration was feasible for maximum 200 W.

The SI-200 architecture was suitable for small satellites where the accommodation of earth observation and/or science payload was required. SI-200 platform was designed to satisfy the mission requirements by incorporating three-axis stabilized, accurate and agile attitude control for precise imaging operations. Dual redundancies were adapted where necessary in the system architecture design to increase the reliability of the satellite system.

The SI-200 platform, 1.2 m in diameter and 1.35 m in height, featured deck-and-longeron type structure permitting easy assembly and disassembly. The interface with the launch vehicle was made through an adapter bolted to the bottom of the structure. The mechanical interface with the electro-optical payload was provided through three points at the satellite middle deck.

Mass: < 200 kg; Power Generation: 330 W @ EOL, 3 deployable panels.

More at: Razaksat.

Family: Surveillance. Country: Korea South. Launch Vehicles: Dnepr, Falcon 1. Launch Sites: Baikonur LC109, Kwajalein OM. Bibliography: 13065.

Photo Gallery

	Dubaisat 1Credit: Manufacturer Image

2009 July 14 - . 03:36 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein OM. LV Family: Falcon. Launch Vehicle: Falcon 1.

Razaksat - . Mass: 180 kg (390 lb). Nation: Malaysia. Agency: SpaceX. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: Satrec. USAF Sat Cat: 35578 . COSPAR: 2009-037A. Apogee: 690 km (420 mi). Perigee: 665 km (413 mi). Inclination: 9.00 deg. Period: 98.30 min. Malaysian imaging satellite..

2009 July 29 - . 18:46 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. LV Family: R-36M. Launch Vehicle: Dnepr.

Dubaisat 1 - . Mass: 190 kg (410 lb). Nation: UAE. Agency: Makeyev bureau. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: SatRec. USAF Sat Cat: 35682 . COSPAR: 2009-041B. Apogee: 682 km (423 mi). Perigee: 666 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. Emirates Institute of Advanced Science and Technology, Dubai..

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z