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Latest launch:

Date: 6 September 2007
Launch vehicle:"Proton-M"
Spacecraft: "JCSat-11"
Site:Baikonur

 

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Date:  
Launch vehicle: "Proton-M"
Spacecraft:
Site: Baikonur

Rambler's Top100

JCSAT 11 Mission Booklet
JCSAT 11 Mission Booklet
Booklet DIRECTV 10
Фотоальбом
KHRUNICHEV`S HYSTORY
1, 2, 3, 4, 5, 6.





  20.09.2007 * ILS Press Release
ILS Establishes Failure Review Oversight Board For JCSAT-11 Mission. Подробно

  19.09.2007 *Press-release
Preparations Under Way for Angara Booster Fire Tests Подробно








 

 

 

 
 

Фото         FGB-based Multipurpose Lab Module (MLM).
   The effort to build FGB 2 as a back-up for FGB 1 dates back to 1995 when the top managers of the Khrunichev Space Center decided to engage in this project using the Center’s budget, almost in parallel with creating the Functional Cargo Module Zarya, the first element of the ISS.

Main Specifications .

Liftoff mass

20300 kg

Parking orbit :
max Altitude
min Altitude
Inclination


350 km
185 km
51,6 0

Main Functions .

    - Provide a port to dock a supply vehicle or a research modul
    - Provide transit lines to deliver propellants from the Progress re-supply vehicle to the Zvezda Service Module
   - Accommodate a power distribution system to collect and condition output power of the four high-voltage solar panels mounted at the modified Science-and- Power Platform.
   - Provide stowage space.
    - Accommodate, and support functioning of, the European Robotic Arm (ERA).
   - Accommodate, and support functioning of, research instruments.
    - Accommodate Space Shuttle-delivered stowage platform.

Potential Commercial Applications :

  • Provide stowage capacities
  • Deliver cargo to orbit
  • Provide services related to transmission, storage or processing of payload output data
  • Provide a downlink channel
  • Grow available power by adding new solar arrays
  • Provide interfaces to internal payloads
  • Provide interfaces to external payloads
  • Support air lock operations involving payloads
  • Accommodate and ensure functioning of a life support system for a 3-strong crew
  • Accommodate living quarters

Functions to Support Russian Segment

  • Control roll maneuvers
  • Provide a port to attach supply vehicles
  • Deliver the ERA to orbit, provide space to position ERA connection points during extra-vehicular activities (EVA) and support ERA on-orbit operations

Description .

    The effort to build FGB 2 as a back-up for FGB 1 dates back to 1995 when the top managers of the Khrunichev Space Center decided to engage in this project using the Center’s budget, almost in parallel with creating the Functional Cargo Module Zarya, the first element of the ISS.
    In compliance with Rosaviacosmos Decision dated February 16, 2004, on “Implementation of abbreviated ISS configuration” approved by Yu.N. Koptev, Director General, Rosaviacosmos, as well as the Federal Space Agency Decision dated July 20, 2004, on “Multipurpose Lab Module (MLM) implementation process 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.
    The target date for the completion of MLM as defined in the MLM Program Schedule is late 2007. At present, the MLM’s detailed profile has been finalized based on streamlined design parameters proceeding from the need to reduce the cost and time to be spent on building the Russian Segment of the ISS while making the most of the hardware backlog and potential investment from foreign partners and commercial customers. Following final definition of the MLM Design Specification within the abbreviated Russian Segment configuration of the ISS, it will take two years to implement modifications.
    As per the ISS RS abbreviated configuration the FGB 2-based MLM is to support further ISS RS deployment providing docking ports to transportation vehicles and research modules as well as accommodating payloads, providing stowage capability, etc.
    The MLM should be capable of supporting commercial projects to the degree possible so as to outsource off-budget funding including investments to be used to complete and commission the module.
    Following are the requirements set for the FGB 2-based MLM as derived from the input data:
   1. Provide a port for Soyuz-TM, Progress-M Vehicles and their modifications as well as for research modules to be able to dock in either automatic or manual (TORU – Teleoperator Control Mode) mode.
   2. Support propellant transfer from Progress Vehicles into the SM and FGB tanks.
   3. Support the ISS attitude control with regard to roll using its own jets.
    4. Provide room to accommodate ERA Robotic Arm, provide footprints for external experiments and for a cargo pallet, install probes for stowage and maintenance of the upmassed payloads.


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