
Khrunichev Space R&D Center
Khrunichev Space Center is located in Russia. It is the famous manufacturer of the Proton Rocket and Rockot. Khrunichev is also developing the Angara Launch Vehicle.
The Khrunichev State Research and Production Space Centre was created by an RF presidential decree of 7 June 1993 on the base of the largest producers of aerospace and rocket technology: the Khrunichev Machine-building Plant and the Salyut Design Bureau. Khrunichev State Research and Production Space Centre is one of the world's largest aerospace corporations leading the international market of space services.
Khrunichev
State Research and Production Space Center manufactured all the Russian manned
orbital stations: 'Salyut', 'Mir' and 'Almaz' and also all the heavy modules
that docked to the orbital stations and the three-seater recoverable
spacecrafts. First generation orbital stations 'Salyut', 'Salyut 2', 'Salyut-3',
'Salyut-4' and 'Salyut-5' had only one docking port. This essentially limited
the manned flight possibilities. The second generation orbital stations
('Salyut-6' and 'Salyut-7') had two docking units which significantly expanded
the stations' operation capabilities. An important stage in provisioning of the
'Salyut-6' and 'Salyut-7' stations' operation was the use of "Kosmos" ferry
spacecraft. The Center manufactured four such spacecrafts: "Kosmos-929",
"Kosmos-1267", "Kosmos-1443" and "Kosmos-1686".
The creation of the automatic unmanned orbital station "Almaz" was an important step in spacecraft development. The first 'Kosmos-1870' was in orbit from July 25, 1987 to July 30, 1989. The high quality radar imagery of the Earth's surface, obtained from this station, was used in the interests of the Ministry of Defense and national economy. "Almaz-1" with modernized radar, allowing to obtain high spatial resolution images of the Earth, was in orbit from March 31,1991 to October 17,1992.
Polyus
The experimental spacecraft "Polyus" of 100-ton class was developed on the basis of FCM (functional cargo module) using the modular design. It served as a payload during the first launch of the "Energiya" launcher on May 15,1987. Polyus spacecraft served as a dimension and mass mock-up during the flight of Energiya.
Mir Space Station
Mir Space Station, the multi-purpose permanent orbital complex was a third generation station. Its purpose was the realization of the Russian national space scientific program, the practical solution of various economic tasks and for joint work in international programs on contractual and commercial basis. The basic module - the orbital station "Mir" was launched on February 20,1986. The station had two docking ports where "Soyuz" spacecraft - delivering and changing crews and various unmanned modules including "Progress" ferries could dock to. One of the docking ports had a device which made it possible for re-docking of the docked modules to the four-side docking adapter and their stay in a fixed position during operation of the station "Mir". The basic module's construction has allowed to create a multi-purpose, modular type manned complex in space for the first time.
The astrophysical module "Kvant" was launched on March 31, 1987 and in ten days it docked to the "Mir" station. Then in five days a part of the module carrying auxiliary systems separated from the station's scientific module and after 135 days of independent flight burnt in the atmosphere dense layers. The astrophysical module "Kvant" is a multipurpose one. It includes astrophysical instrumentation, an electrophoretic plant for obtaining super-pure biologically active substances in zero gravity, equipment for visual observation of the Earth's surface and auxiliary and experimental equipment supplementary to the "Mir" station onboard systems. There was a spacious pressurized working compartment for astronauts.
In December 1989 the module "Kvant-2" joined the station. Its purpose was to additionally equip "Mir" with astronaut life support systems and to increase the orbital complex's power capabilities. The module carried load-bearing gyro attitude control systems, power supply systems, new plants for obtaining oxygen and for water regeneration and domestic appliances.
In July 1990 the module "Kristall" was docked to the complex. Its purpose was to carry out tests of new technologies for pro-ducing construction materials, semi-con-ductors and improved bio-agents, in zero gravity. The "Kristall" module's androgynous docking unit is designed for docking with reusable "Buran" and "Shuttle" type spacecrafts.
The assembly of "Mir" complex was continued in
1995.
On June 1, 1995 the complex was supplemented with the "Spektr" research module.
It was integrated into the "Mir" complex in order to research the Earth's
natural resources, the upper layer of the atmosphere, near station space,
geophysical natural and artificial processes in the near-Earth space and in the
upper layers of the atmosphere and to perform medical and biologic; studies on
the joint Russian-American programs "Mir - Shuttle" and "Mir - NASA". It also
equipped the station with additional power supply sources. Additionally the
module "Spektr" was used as a supply ferry. It delivered fuel supplies,
expendable materials and additional equipment to the station "Mir". The assembly
of "Mir" was completed in 1996, when the Earth remote sensing module "Priroda"
joined the station.
International Launch Services
The
Lockheed-Khrunichev-Energia joint venture was registered on April 15, 1993. The
Russian participants was the Khrunichev State Research and Production Space
Center and the Energia Rocket Space Corporation. The US particirants was
Lockheed company. As a result of the joint venture’s activities the Proton
launcher has begun to appear on the world market. In 1994 the two US companies
Lockheed and Martin Marietta amalgamated and formed Lockheed – Martin. The
logical continuation of the activities of the joint venture Lockheed-Khrunichev-Energia
was the creation in June 1995 of the joint venture International Launch Services
(ILS). ILS offers telecommunications satellite launch services in the world
market, using the Atlas launch vehicle family (manufactured by Lockheed-Martin,
a U.S. company) or the Proton-K LV, the Proton-M LV or the Angara LV families
(manufactured by the Khrunichev Space Center, a Russian company).
The “Proton-K” launcher is a whole era in the development of Soviet launch vehicles. However some of the “Proton-K” parameters were improved – the control system and some of operational characteristics, were increased the space for payload accommodation.
Proton M’s new payload fairing accommodates larger payloads and advanced upper stage boosters. One such booster is the Breeze M (it is the upper stage booster that supports the final phase of injection into a target orbit). The Breeze M upper stage makes it possible to increase the payload-to-GTO mass to 6 tons. Breeze-M had its international debut on December 30, 2002 when Proton-M launched the Nimiq-2 telecommunications satellite.
Angara
Khrunichev
Space Center is developing an oxygen-hydrogen booster (OHB). The booster will
significantly improve the Proton-M’s energy and mass characteristics and will
make possible to expand the rage of tasks on the injection of various
spacecraft. In August 1994 Khrunichev State Space Center was announced the
winner in the competition for creation of the space rocket complex "Angara". As
part of the Angara program, Khrunichev is implementing a strategy of expeditious
development of a common core booster powered by LOX/kerosene engines to serve as
the basis for a number of advanced environment-friendly launchers of small-,
medium- and heavy-lift classes. Underpinning the Angara project is the idea to
secure Russia’s assured access to space from the Russian launch base at Plesetsk
and guarantee that Russia will be able to engage in space activities regardless
of any trends in military-political and economic relations with other countries.
The launch complex "Angara" will be situated at Plesetsk. On December 22, 2004
an inter-governmental agreement was signed between the Russian Federation and
Republic of Kazakhstan on the Development of the Baiterek Space Launch Complex
at the Baikonur Cosmodrome. The Agreement lays down fundamental principles and
terms of collaboration in the development and joint use at Baikonur of Baiterek,
a new environment-friendly space launch complex. Under the Baiterek project, new
processing and launch facilities will be built at Baikonur to support launches
of the Angara launch vehicle.
Baikal
Baikal
is a future reusable launch vehicle (RLV) being developed jointly by KhSC and
the Molniya (‘Lightning’) Research and Production Corporation. The purpose of
this project is to reduce the operational launch vehicle cost and to minimize
the drop fields, a problem of extreme significance now that the Russian launch
bases are located well inside a continent. Thus if the RLV integrated in an
Angara launcher lifted off at Plesetsk, Russia then on its back flight this
return vehicle might land onto the Plesetsk airfield. In accordance with the
Agreement on strategic armaments reduction a number of Russian intercontinental
ballistic missiles are to be destroyed. They include the SS-19 rocket. Within
the framework of the conversion program Khrunichev State Research and Production
Space Center is creating the "Rockot" launcher on the basis of this missile. The
"Rocket's" technical characteristics allow to launch spacecrafts into low,
middle circular and elliptic orbits (including high elliptic orbits). The
“Rockot” launcher includes the third stage - the "Breeze-KM" booster. The
"Breeze-KM" booster's main engine is able to multiple ignite. This allows to
realize different schemes of S/C delivery into orbit together with a piggy-back
launch of several S/Cs into one or several various orbits. The "Breeze-KM"
booster instrumentation is able to provide high accuracy of S/C injection into
the orbit, and, if necessary, its power sup-ply during flight of up to 7 hours.
The Eurockot company was set up jointly by the Khrunichev Space Center (KhSC)
and Produktbereich Raumfahrt Infrastruktur, a division of Deutsche Aerospace AG
(DASA), the Joint Venture Agreement having been signed on May 16, 1994. At
present, KhSC owns 49% of the Eurockot stock and EADS Space Transportation owns
51%.
The 12KRB upper stage was developed and fabricated by the Khrunichev Space Center for GSLV, a new Indian launch vehicle, under a contract with the Indian Space Research Organization (ISRO). 12KRB is used as GSLV's third stage. Its sustainer developed by the Isaev Chemical Machine Building Design Bureau is a cryogenic engine using liquid propellants (namely, the liquid oxygen and the liquid nitrogen). When integrated in GSLV the 12KRB upper stage can inject an up to 2500-kg spacecraft into geotransfer orbit from Sriharikota-SHAR, the Indian launch center.
A first successful launch of GSLV with 12KRB as a cryogenic upper stage took place on April 18, 2001 . On October 26, 2004 a contract was signed to design and build a Space Rocket Complex with a small-lift Launch Vehicle KSLV 1. The design represents a joint effort: KhSC will build the 1st KSLV 1 Stage while the 2nd Stage is to be designed and produced in South Korea . The Contract with the Republic of Korea to develop a Space Rocket Complex with a small-lift Launch Vehicle KSLV 1 for this country has been the result of a long (more than two years) and effort-consuming exercise.
International Space Station
Khrunichev Space Center's participation in the
ISS program is a logical continuation of work on creation of orbital stations.
Khrunichev Center is developing and manufacturing the first element of the
International Space Station (ISS) - the Functional Cargo Module (FCM) Zarya, and
Service Module. The Zarya module was successfully placed in orbit by a Proton
Launch Vehicle on November 20, 1998 .The Service Module, which was being
developed and designed by Khrunichev virtually in parallel with the Zarya block,
is a considerably modified version of the Mir core module. A Proton K launcher
carrying Zvezda ('Star'), was successfully launched from Baikonyr on July 12,
2000.
While KhSC were developing Zarya a decision was made by KhSC managers in 1995 to
finance and build FGB2, a Zarya backup, that might eventually be incorporated in
the Russian segment of the ISS. In compliance with Rosaviacosmos Decision dated
February 16, 2004 , on “Implementation of abbreviated ISS configuration”
approved by Yuri Koptev, Director General, Rosaviacosmos, as well as the Federal
Space Agency Decision dated July 20, 2004 , on “Multipurpose Lab Module (MLM)
implementation pr ocess using the FGB 2 backlog”, approved by A.N. Perminov, the
Head of the Federal Space Agency, the MLM was included in the Russian Segment
Configuration on the nadir port of Zarya Module.
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Updated: Saturday 28th, September, 2010