Manufacturer | Boeing | ||
---|---|---|---|
Production | |||
Status | In service | ||
On order | 84 | ||
Launched | 76 | ||
Lost | 8 | ||
Maiden launch | Optus B1 13 August 1992 | ||
Last launch | TDRS-M 18 August 2017 | ||
Related spacecraft | |||
Derivatives | Boeing 601HP [1] | ||
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The Boeing 601 (sometimes referred to as the BSS-601, and previously as the HS-601) is a retired communications satellite bus designed in 1985 and introduced in 1987 by Hughes Space and Communications Company. The series was extremely popular in the 1990s, with more than 84 purchased by customers globally. The more advanced 601HP derivative (for "high power") was introduced in 1995. [1] Hughes, and the 601 platforms, were acquired by Boeing in 2000.
The last commercial 601 satellite was ordered in 2001 and launched in 2004. The NASA Space Communications and Navigation (SCaN) Program Office in December 2007 selected the BSS-601HP for its third generation TDRS spacecraft, adding the two 15-foot (4.5m) diameter steerable antennas. The TDRS-M satellite, launched on August 18, 2017, became the last 601 satellite to reach orbit. [2]
The Boeing-601 model was Hughes’ first major design and development for a communications satellite with three-axis, or body stabilization. All previous Hughes satellite models (HS-376) had been cylindrical spacecraft that were spin-stabilized at 50 revolutions per minute. Design of the Boeing-601 began in 1985, with full-scale development following two years later. The new satellite's first official public presentation took place at the Telecom 87 conference in Geneva, Switzerland.
The 601 bus is divided into two modules. The first module houses the propulsion system, batteries, and electronics for the bus, and bears launch vehicle loads. The second module contains shelves carrying the communications equipment, payload electronics, and heat pipes. Solar arrays, reflectors, and antenna feeds are mounted to the payload module. [3]
The standard 601 platform supports up to 48 transponders and provides up to 4,800 watts of power. The 601HP supports up to 60 transponders and provides up to 10,000 watts. [3]
A significant number of Boeing 601s have experienced failures in orbit, some resulting in complete failure of the satellite. [4] [5]
An unconfirmed number of 601s launched prior to August 1997 have a design flaw in their SCPs, where a tin-plated relay forms crystalline "whiskers" under certain specific conditions. These whiskers eventually caused an electrical short. Each satellite contains two SCPs and the backup unit will take control in the event of a failure of the primary unit. In some cases, both SCPs have failed, rendering the spacecraft unusable. A notable example was the Galaxy IV satellite. [6] At least eight 601s have experienced SCP failures; four of which were double failures resulting in total loss of the satellite. [7] Hughes switched to nickel plating on later 601s to resolve this problem, at the expense of payload weight. [6]
Some 601HPs have experienced problems with their batteries, resulting in a reduction of eclipse protection. This would require some transponders to be shut down during eclipse periods. [8] [9]
Some Boeing-601 satellites featured the optional electronic propulsion system, called Xenon Ion Propulsion System or XIPS, for station keeping. At least four satellites with XIPS propulsion have experienced partial or total failure of the XIPS system which significantly reduced the lifespan of the satellite. [4]
Latest operator | Satellites [3] |
---|---|
APT Satellite | Apstar 2 (destroyed in launch accident, January 1995) |
Asia Satellite Telecommunications Company | AsiaSat 3S AsiaSat 4 |
DirecTV | DIRECTV 1 DIRECTV 2 DIRECTV 3 DIRECTV 1R DIRECTV 4S |
Indosat | Palapa C1 (launched January 1996) Palapa C2 (launched May 1996) |
Intelsat | Intelsat 2 (launched July 1994) Intelsat 3R (launched January 1996 as PAS-3R) Galaxy 4R (601HP; launched April 2000; originally operated by PanAmSat, which was later acquired by Intelsat) Intelsat 5 (601HP; launched August 1997; known variously as IS-5, PAS-5, and Arabsat 2C) Intelsat 9 (601HP; launched July 2000 as PAS-9 operated by PanAmSat) Galaxy 10R (601HP; launched January 2000) |
JSAT Corporation | JCSAT-3 (launched August 1995) JCSAT-4 (launched February 1997) JCSAT-5 (launched December 1997) JCSAT-4A (launched February 1999; formerly designated JCSAT-6) JCSAT-8 (launched March 2002) |
Loral Space & Communications | Orion 3 (601HP; launched May 1999; failed to achieve correct orbit) |
MEASAT | MEASAT-3 (launched December 12, 2006) |
NASA | TDRS-H (launched June 2000) TDRS-I (launched March 2002) TDRS-J (launched December 2002) TDRS-K (601HP; launched January 2013) TDRS-L (601HP; launched January 2014) TDRS-M (601HP; launched August 2017) |
NOAA/NASA | GOES N GOES O GOES P |
Optus (formerly AUSSAT) | Optus B1 (launched August 1992) Optus B2 (launched December 1992; launch failure) Optus B3 (launched August 1994) |
PanAmSat | Galaxy IIIR Galaxy IV Galaxy VI Galaxy VIR (601HP) Galaxy VIIIi (601HP) Galaxy X (601HP) Galaxy XR (601HP) PAS-2 (launched July 1994) PAS-3 (launched December 1994; launch failure) PAS-3 (spare satellite launched January 1996; re-designated PAS-3) PAS-4 (launched August 1995) PAS-5 (601HP, launched August 1997; first 601 HP to launch) PAS-6B (launched December 1998) PAS-10 (launched May 2001) PAS-22 (launched as AsiaSat 3; later sold to Hughes Communications and re-designated HGS-1; then sold to PanAmSat and re-designated PAS-22) |
Pendrell Corporation (formerly ICO Global Communications) | (Twelve satellites in MEO) |
Satmex | Solaridad 1 (launched November 1993) Solaridad 2 (launched October 1994) Satmex 5 (601HP; launched December 1998) |
SES S.A. | Astra 1C Astra 1D Astra 1E Astra 1F Astra 1G Astra 2A Astra 1H Astra 2C SES-7 (launched May 2009 as ProtoStar 2 for ProtoStar Ltd; later sold to SES) |
SKY Perfect JSAT Group (formerly Space Communications Corporation) | Superbird-C (launched July 1997) Superbird-B2 (601HP; launched February 2000; previously designated Superbird-4) Superbird-6 (launched April 2004) |
TerreStar Corporation (formerly Motient Corporation, American Mobile Satellite Corporation) | AMSC-1 (launched April 1995) |
TMI Communications | MSAT-1 (launched April 1996) |
United States Navy | Eleven UHF Follow-On spacecraft designated F1-F11 (launched between 1993 and 2003) |
Galaxy IV was a model HS-601 satellite built by Hughes Space and Communications Company (HSC). The satellite, which carried a payload of both C band and Ku band transponders, was launched on June 24, 1993 and operated by PanAmSat Corporation. It was in geostationary orbit at 99°W.
Boeing 702 is a communication satellite bus family designed and manufactured by the Boeing Satellite Development Center, and flown from the late-1990s into the 2020s. It covers satellites massing from 1,500 kg (3,300 lb) to 6,100 kg (13,400 lb) with power outputs from 3 to 18 kW and can carry up to approximately 100 high-power transponders.
A satellite bus is the main body and structural component of a satellite or spacecraft, in which the payload and all scientific instruments are held.
TDRS-8, known before launch as TDRS-H, is an American communications satellite, of second generation, which is operated by NASA as part of the Tracking and Data Relay Satellite System. It was constructed by Boeing and is based on the BSS-601 satellite bus.
Eurostar is a satellite bus made by Airbus Defence and Space which has been used for a series of spacecraft providing telecommunications services in geosynchronous orbit (GEO). More than 70 Eurostar satellites have been ordered to date, of which more than 55 have been successfully launched since October 1990 and have proven highly reliable in operational service. In December 2013, the Eurostar satellites accumulated 500 years of successful operations in orbit. The Eurostar spacecraft series is designed for a variety of telecommunications needs including fixed services and broadcast, mobile services, broadband and secured communications.
TDRS-11, known before launch as TDRS-K, is an American communications satellite which is operated by NASA as part of the Tracking and Data Relay Satellite System. The eleventh Tracking and Data Relay Satellite is the first third-generation spacecraft.
TDRS-12, known before launch as TDRS-L, is an American communications satellite operated by NASA as part of the Tracking and Data Relay Satellite System. The twelfth Tracking and Data Relay Satellite, it is the second third-generation spacecraft to be launched, following TDRS-11 in 2013.
BSAT-1a was a geostationary communications satellite designed and manufactured by Hughes on the HS-376 platform. It was originally ordered and operated by the Broadcasting Satellite System Corporation (B-SAT). It was used as the main satellite to broadcast television channels for NHK and WOWOW over Japan. It had a pure Ku band payload and operated on the 110°E longitude until it was replaced, along its backup BSAT-1b, by BSAT-3a. On 3 August 2010, it was decommissioned and placed on a graveyard orbit.
TDRS-13, known before launch as TDRS-M, is an American communications satellite operated by NASA as part of the Tracking and Data Relay Satellite System. The thirteenth Tracking and Data Relay Satellite, it is the third and final third-generation spacecraft to be launched, following the 2014 launch of TDRS-12.
BSAT-1b was a geostationary communications satellite designed and manufactured by Hughes on the HS-376 platform. It was originally ordered and operated by the Broadcasting Satellite System Corporation (B-SAT). It was used as backup of BSAT-1a to broadcast television channels for NHK and WOWOW over Japan. It had a pure Ku band payload and operated on the 110°E longitude until it was replaced, along its twin BSAT-1a, by BSAT-3a.
Superbird-A2, known as Superbird-6 before launch, was a geostationary communications satellite ordered and operated by Space Communications Corporation (SCC) that was designed and manufactured by Hughes on the BSS-601 satellite bus. It had a mixed Ku-band and Ka-band payload and was expected replace Superbird-A at the position at 158° East longitude. It was expected to provided television signals and business communications services throughout Japan, South Asia, East Asia, and Hawaii.
Horizons-1, also known as Galaxy 13, is a geostationary communications satellite operated by Intelsat and SKY Perfect JSAT (JSAT) which was designed and manufactured by Boeing on the BSS-601 platform. It has Ku-band and C-band payload and was used to replace Galaxy 9 at the 127.0° West longitude. It covers North America, Puerto Rico, Alaska, Hawaii and Mexico.
JCSAT-1B, known as JCSAT-5 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Hughes on the HS-601 satellite bus. It has a pure Ku-band payload and was used to replace JCSAT-1 at the 150° East longitude. It covers Japan, Korea, most of China, Thailand, Vietnam, Laos, part of Indonesia, part of Malaysia and Hawaii.
JCSAT-4 was known as JCSAT-R until it was sold to Intelsat in 2009. It is a geostationary communications satellite designed and manufactured by Hughes on the HS-601 satellite bus. It was originally ordered by JSAT Corporation, which later merged into the SKY Perfect JSAT Group. It has a mixed Ku-band and C-band payload and was used as an on orbit spare.
JCSAT-3 was a geostationary communications satellite designed and manufactured by Hughes on the HS-601 satellite bus. It was originally ordered by JSAT Corporation, which later merged into the SKY Perfect JSAT Group. It has a mixed Ku-band and C-band payload and operated on the 128° East longitude until it was replaced by JCSAT-3A.
JCSAT-1 was a geostationary communications satellite designed and manufactured by Hughes on the HS-393 satellite bus. It was originally ordered by Japan Communications Satellite Company (JCSAT), which later merged into the JSAT Corporation. It had a Ku-band payload and operated on the 150° East longitude until it was replaced by JCSAT-1B.
JCSAT-2 was a geostationary communications satellite designed and manufactured by Hughes on the HS-393 satellite bus. It was originally ordered by Japan Communications Satellite Company (JCSAT), which later merged into the JSAT Corporation. It had a Ku-band payload and operated on the 154° East longitude until it was replaced by JCSAT-2A.
SBS 6 was a geostationary communications satellite designed and manufactured by Hughes on the HS-393 platform. It was originally ordered by Satellite Business Systems, which later sold it to Hughes Communications and was last used by Intelsat. It had a Ku band payload and operated on the 95°W longitude.
The Hughes 393 is a communications satellite bus introduced in 1985 by Hughes Space and Communications Company. It was a spin-stabilized bus that had twice as much power as the HS-376 platform.
Superbird-C, also known as Superbird-3 or Superbird-A3, was a geostationary communications satellite ordered and operated by Space Communications Corporation (SCC) that was designed and manufactured by Hughes Space and Communications Company on the HS-601 satellite bus. It has a pure Ku-band payload and was used to fill the position at 144° East longitude. It provided television signals and business communications services throughout Japan, South Asia, East Asia, and Hawaii.