|
DS-2000
The DS2000 is a geostationary communications satellite bus designed and manufactured by Mitsubishi Electric of Japan. Designed to carry payloads between and , with power requirements of up to 15 kW. It is compatible with Ariane 5, Proton-M, Zenit-3SL, Atlas V, Falcon 9 and H-IIA. According to Moog-ISP, the DS2000 platform uses its bipropellant thrusters. List of satellites Satellites using the DS2000 platform. See also * A2100 – Similar satellite bus made by Lockheed Martin Space Systems and popular with Japanese satellite operators * SSL 1300 – Another comparable satellite bus used by Japanese satellite operators and made by SSL References {{Reflist, 30em, refs= {{cite web , url=http://www.astronautix.com/d/ds2000.html , archive-url=https://web.archive.org/web/20160820094902/http://www.astronautix.com/d/ds2000.html , url-status=dead , archive-date=August 20, 2016 , last=Wade , first=Mark , title=DS2000 , access-date=2016-07-29 {{cite web , last1=Krebs , first1= ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Himawari 9
Himawari 9 is a Japanese weather satellite, the 9th of the Himawari geostationary weather satellite operated by the Japan Meteorological Agency. The spacecraft was constructed by Mitsubishi Electric, and is the second of two similar satellites to be based on the DS-2000 bus. Launch Himawari 9 was launched on 2 November 2016, 06:20:00 UTC, atop a H-IIA rocket flying from the Yoshinobu Launch Complex Pad 1 at the Tanegashima Space Center, and by 11 November 2016 it reached to the geostationary point at 140.7 degrees East. After initial function tests, it was put on standby until 05:00 UTC by 13 December 2022, when it succeeded Himawari 8 is a Japanese weather satellite, the 8th of the Himawari geostationary weather satellites operated by the Japan Meteorological Agency. The spacecraft was constructed by Mitsubishi Electric with assistance from Boeing, and is the first of two .... The launch was scheduled initially on 1 November 2016, but postponed for one day due to th ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
DSN-2
DSN-2, also known as Kirameki-2, is a geostationary orbit, geostationary communications satellite to be operated by DSN Corporation, a subsidiary of SKY Perfect JSAT Group. Its payload is a pure X band, X-band and will be used for military communications by the Japan Self-Defense Forces, Japanese military. It was launched and successfully deployed on 24 January 2017 using a H-IIA rocket flying in its heaviest configuration, the H-IIA 204. It is Japan's first dedicated military communication satellite and is designed for at least fifteen years of service. History JSAT Corporation, JSAT along NEC, NTT Communications and Maeda Corporation formed a joint venture called DSN Corporation. On 15 January 2013, DSN Corporation announced that it had closed a contract with the Ministry of Defense (Japan), Ministry of Defense to execute the "Program to Upgrade and Operate X-Band Satellite Communications Functions, etc". The contract is a private finance initiative, where private funds, mana ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
ST-2
''ST-2'' is a telecommunications satellite made by Mitsubishi Electric. It was launched on May 20, 2011 atop an Ariane 5 ECA rocket from ESA's Guiana Space Centre in a dual-launch mission with GSAT-8. a ST-2 is a replacement for the ST-1 satellite. It is built around the DS2000 spacecraft bus. It is in geosynchronous orbit at 88 deg. East, and is operated by the ST-2 Satellite Ventures joint company of Singapore Telecommunications(SingTel) and Chunghwa Telecom Chunghwa Telecom Company, Ltd. () (, ) is the largest integrated telecom service provider in Taiwan, and the incumbent local exchange carrier of PSTN, Mobile, and broadband services in the country. History Chunghwa Telecom was founded as .... It provides relay services over the Middle East, Central Asia, India and Southeast Asia. References External links * http://www.arianespace.com/press-release/arianespace-launch-for-asia-and-india-st-2-and-gsat-8-satellites-in-orbit/ * https://web.archive.org/web/2012 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
ETS-VIII
JAXA Engineering Test Satellite ETS-VIII (Kiku 8) is the eighth technology test satellite in a series which started with ETS-1 in 1975 by NASDA. It was launched with the H-2A on December 18, 2006. ETS-VIII was developed by JAXA in cooperation with NICT and NTT. The aim of ETS-VIII is to enable satellite communications with small terminals. Unlike the Iridium satellites for mobile communication, ETS-VIII is positioned at GEO. However to fulfill the task the satellite must carry two very large antennas. It was the first use of the 204 configuration (four strap-on boosters) of the H-IIA launch vehicle. Timetable *December 20, 2000: Launch of LDREX, a demonstration of the large antenna reflector deployment, aboard Ariane 5. Deployment failed. *October 14, 2006 Launch of LDREX-2 with the Ariane 5 Ariane 5 is a European heavy-lift space launch vehicle developed and operated by Arianespace for the European Space Agency (ESA). It is launched from the Centre Spatial Guyanais (C ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Bipropellant Rocket
A liquid-propellant rocket or liquid rocket utilizes a rocket engine that uses liquid propellants. Liquids are desirable because they have a reasonably high density and high specific impulse (''I''sp). This allows the volume of the propellant tanks to be relatively low. It is also possible to use lightweight centrifugal turbopumps to pump the rocket propellant from the tanks into the combustion chamber, which means that the propellants can be kept under low pressure. This permits the use of low-mass propellant tanks that do not need to resist the high pressures needed to store significant amounts of gasses, resulting in a low mass ratio for the rocket. An inert gas stored in a tank at a high pressure is sometimes used instead of pumps in simpler small engines to force the propellants into the combustion chamber. These engines may have a higher mass ratio, but are usually more reliable, and are therefore used widely in satellites for orbit maintenance. Liquid rockets can be mono ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Türksat 4B
Türksat 4B is a Turkish communications satellite, operated by Türksat. Overview According to the in-orbit delivery contract signed in early 2011, Mitsubishi Electric (MELCO) of Japan was in charge of the construction of the satellite's base MELCO DS2000, and the American-Russian joint-venture company International Launch Services (ILS) provided the launch of the spacecraft atop a Russian Proton-M space launch vehicle from Baikonur Cosmodrome in Kazakhstan scheduled in late 2014. In the scope of the contract, Turkish engineers collaborated in the production of the satellite. The production of Türksat 4B at the Mitsubishi Electric Facility in Kamakura was completed in June 2014. Türksat 4B is part of the Turksat series of satellites, and is placed in geosynchronous orbit at 50°E to provide telecommunication and direct TV broadcasting services over a wide geographic region between west of China and east of England spanning Turkey, as well as Europe, Central Asia, the M ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Briz-M
The Briz-K, Briz-KM and Briz-M (russian: Бриз-К, КM and M meaning ''Breeze-K, KM and M'') are Russian liquid-propellant rocket orbit insertion upper stages manufactured by Khrunichev State Research and Production Space Center and used on the Proton-M and Angara A5. The upper stages were also used on Rokot, one of Russia's smaller launchers, before its retirement in 2019. Characteristics Briz-K and Briz-KM Briz-K, GRAU index 14S12, is a single-piece structure with a conical tank compartment and the engine located in a recess in the fuel tank. Briz-KM (GRAU index 14S45) is an improved version of Briz-K. The Briz-K and Briz-KM were used as a third stage of the Rokot launch vehicles. Briz-M Briz-M, GRAU index 14S43, is designed for injecting large payloads into a low, medium-height or high geosynchronous orbit. Briz-M is a twin upper stage consisting of a core module (using Briz-KM as the baseline) and a jettisonable add-on toroidal tank surrounding the core. It is ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Türksat 4A
Türksat 4A is a Turkish communications satellite, operated by Türksat. It was constructed by Mitsubishi Electric (MELCO) of Japan, based on the MELCO DS2000 satellite bus, and was launched by the American-Russian joint-venture company International Launch Services (ILS) atop a Russian Proton-M space launch vehicle on February 14, 2014, at 21:09:03 from Site 81/24 of the Baikonur Cosmodrome in Kazakhstan. The in-orbit delivery contract for the satellite was signed in March 2011. In the scope of the contract, Turkish engineers were trained in the facilities of MELCO in Japan. During the official visit of Prime Minister Recep Tayyip Erdoğan to Japan, the satellite was handed over by the Mitsubishi Electric to the Turkish officials in a ceremony on January 8, 2014. The initially planned launch date of Türksat 4A in November 2013 was postponed to February 2014 due to the suspension of the Proton-M launches because of problems, which arose on December 8, 2012. Türksat 4A is ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Himawari 8
is a Japanese weather satellite, the 8th of the Himawari geostationary weather satellites operated by the Japan Meteorological Agency. The spacecraft was constructed by Mitsubishi Electric with assistance from Boeing, and is the first of two similar satellites to be based on the DS2000 satellite bus. Himawari 8 entered operational service on 7 July 2015 and is the successor to MTSAT-2 (Himawari 7) which was launched in 2006. Launch Himawari 8 was launched atop a H-IIA rocket flying from the Yoshinobu Launch Complex Pad 1 at the Tanegashima Space Center. The launch occurred at 05:16 UTC on 7 October 2014 and reached its operational geostationary orbit in October 2014, at 35,786 kilometers and 140.7 degrees East. Himawari 9, which is identical to Himawari 8, was launched on 2 November 2016 and placed in a stand-by orbit until 05:00 UTC by 13 December 2022, when it succeeded Himawari 8. Purpose The role of Himawari 8 is to provide typhoon, rainstorm, weather forecast and ot ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Ariane 5 ECA
Ariane 5 is a European heavy-lift space launch vehicle developed and operated by Arianespace for the European Space Agency (ESA). It is launched from the Centre Spatial Guyanais (CSG) in French Guiana. It has been used to deliver payloads into geostationary transfer orbit (GTO) or low Earth orbit (LEO). The launch vehicle had a streak of 82 consecutive successful launches between 9 April 2003 and 12 December 2017. Since 2014, Ariane 6, a direct successor system, is in development. The system was designed as an expendable launch system by the ''Centre national d'études spatiales'' (CNES), the French government's space agency, in cooperation with various European partners. Despite not being a direct derivative of its predecessor launch vehicle program, it is classified as part of the Ariane rocket family. ArianeGroup is the prime contractor for the manufacturing of the vehicles, leading a multi-country consortium of other European contractors. Ariane 5 was originally intended t ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Superbird-C2
Superbird-C2, known as Superbird-7 before launch, is a geostationary orbit, geostationary communications satellite operated by JSAT Corporation and designed and manufactured by Mitsubishi Electric on the DS2000 satellite bus. It had a launch weight of , a 15-year design life and was the first commercial communications satellite built in Japan. Its payload is composed of 28 Ku band, Ku-band Transponder (satellite communications), transponders with a total bandwidth of 828 Hertz, MHz. It was originally ordered by SKY Perfect JSAT, Space Communications Corporation (SCC), but it was later merged and absorbed by JSAT Corporation. By the time of the actual launch it was a fully used Superbird-C2 as a replacement for Superbird-C to provide communications services to Japan, East Asia and the Pacific Ocean. History In April 2005, Space Communications Corporation (SCC) issued an Request for proposal (RFP) for Superbird-7, a spacecraft destined to replace the aging Superbird-C. On 28 Ju ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
