BS 3a, 3b, 3n (Yuri 3a, 3b, 3n) (original) (raw)
Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

BS 3a (Yuri 3a) [NASDA]
The BS-3 or Yuri 3 satellites were a series of Japanese direct broadcasting satellites.
The BS-3 were launched to replace the broadcasting serices of the BS-2, responding to growing broadcasting needs while developing technologies for more advanced broadcasting satellites. They were used for broadcasting and test broadcasting with high-definition television. In 1993, the program was spun off from NASDA to the Broadcasting Satellite System Corporation of Tokyo (B-SAT).
The satellites were based on GE Astro's AS-3000 bus and carried a NEC built broadcasting payload consisting of three active high power Ku-band transponders with three spares.
BS-3a, renamed Yuri 3a, was launched on 28 August 1990 on a Japanese H-1 UM-129A (9 SO) rocket. BS-3a finished its programmed operation on 20 April 1998.
BS-3b, renamed Yuri 3b, was launched about one year later on 25 August 1991 on a Japanese H-1 UM-129A (9 SO) rocket. BS-3b finished its programmed operation on 1 December 1998.
BS-3n or Yuri 3n, was launched on 8 July 1994 on a shared Ariane-44L H10+ launch.
The successor of these satellites were B-Sat's BSat 1a and 1b satellites.
| Nation: | Japan |
|---|---|
| Type / Application: | Communication |
| Operator: | NASDA (#3a, 3b); Broadcasting Satellite System Corporation of Tokyo (B-SAT) (#3n) |
| Contractors: | NEC, RCA Astro → GE Astro → Martin Marietta (Bus) |
| Equipment: | 3 (+3) Ku-band transponders 120W TWTA, 27 MHz bandwidth, EIRP max 54 dBW |
| Configuration: | AS-3000 |
| Propulsion: | Star-30BP (#3n) |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | |
| Mass: | 1100 kg (#3a, 3b) |
| Orbit: | GEO |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| BS 3a (Yuri 3a) | 1990-077A | 28.08.1990 | Ta LP-N | H-1 UM-129A (9 SO) | |
| BS 3b (Yuri 3b) | 1991-060A | 25.08.1991 | Ta LP-N | H-1 UM-129A (9 SO) | |
| BS 3n (Yuri 3n) | 1994-040B | 08.07.1994 | Ko ELA-2 | Ariane-44L H10+ | with PAS 2 |