Concernant le pad Angara à Vostochny voici les détails de l'appel d'offre. On y voit que l'Angara pourra utiliser aussi bien l'étage d'injection Briz-M que le DM.
Le complexe de lancement sera construit par étape: d'abord 1 pad pour les lancements non habités puis 1 pad pour les lancements avec un étage cryotechnique et les vaisseaux habités.
En effet les lancements habités sont prévus dans cet appel d'offre et non dans celui pour le pad soyouz qui ne prévoit que les fusées Soyouz 2.1a, b, v et pas de fusées soyouz 2.3...
3. Tactical and technical requirements
3.1 Composition
3.1.1 SC should consist of two CP common to them with the command post and technological facilities for the operation of these launchers, while preparing to launch space rocket launchers on two simultaneously is not provided.
3.1.2 Start a system must include in its composition:
manufacturing equipment;
Filling RB complex "Breeze-M";
complex automated control systems SC;
set of ground equipment and test equipment RN;
a set of ground equipment and test equipment RB "Breeze-M" (part of a functionally );
a set of ground equipment and test equipment DM (includes functional);
building construction (created from the funds allocated to goskapvlozheniyam);
technical systems (created by the resources allocated to goskapvlozheniyam);
control and test equipment useful load (created at the expense of R & D to create the appropriate payload).
3.1.3 The structure of the process equipment should include:
- starting equipment;
- filling equipment,
- supply equipment;
- Equipment incubation;
- safety equipment;
- control equipment, power supply and control.
3.1.4 Complete set of ground equipment and test equipment must be determined LV leading developer of vehicle and presented to the major creator of SC with the requirements for placement of structures in the latter.
3.1.5 Complete set of ground equipment and test equipment RB "Breeze-M" should be determined by the leading designer and submitted to the said RB head developer of the SC with the requirements for the placement of structures in the latter.
3.1.6 Composition of the set of ground equipment and test equipment DM should be determined by the leading designer and submitted to the said RB head developer of the SC with the requirements for the placement of structures in the last .
3.1.7 The principal building structures should be included (indicated by reference): - two starting structures, - the command post; - facilities to accommodate the technological equipment - facilities to accommodate the complex charging RB "Breeze-M", - access and no-go communication channels; - evaporative area; - Transport communication; - engineering services and network.
3.1.8 The principal technical systems should be included (indicated by reference): power supply system; ventilation and air conditioning installations; water supply and sanitation; system lighting; means of telecommunications and communications; detection and fire fighting; lightning protection system; timing system, established under the ROC "NCI East" (includes functional); engineering and technical means of protection created by goskapvlozheny, and system security and access control, developed in the framework of the ROC, "NCI-East" (includes functional).
3.1.9 Composition of the SC can be updated in the course of OCD.
3.1.10 Composition of systems and components manufacturing equipment must be determined in the course of OCD.
3.1 .11 At the stage of EP leading developer shall develop in accordance with GOST 2.711-82 scheme of division of SK into its constituent parts.
3.1.12 indices IC and its components are assigned to the Customer in accordance with GOST 2.902-68 and the Order of the Federal Space Agency 30.12.2005 № 164 . 3.1.13 The structure of IC should, where appropriate, include sets of equipment monitoring system using satellite navigation technology GLONASS or GLONASS / GPS (available from 13.11.2010 № Roscosmos AL-282).
3.2 Requirements for appointment
3.2.1. When you create a launch pad should be as much as possible be used reserve, created in the performance of work on the IC for ILV "Rus-M" (in terms of the master plan and space-layout decisions buildings SC).
3.2.2. The launch complex is designed to provide prelaunch and launch rockets of the "Angara" light (1.2), medium (A3) and heavy (A5) classes.
3.2.3. The launch complex should be built in stages: creation SC within a single IP, power plants and technology command center in preparation for the launch of space rocket with HGC, includes in its membership RB "Breeze-M" and the DM, as well as automated spacecraft; additional equipment SC second CP to prepare for the launch of space rocket with HGC, includes in its membership other than those listed above, the ACRS and manned spacecraft; upgrade first PU for ILV starts with HGC, includes in its membership ACRS and manned spacecraft.
3.2.4. IC equipment should provide prelaunch preparation and launch of space rocket with a capacity of 10 launches per year with bringing up to 20 launches per year ILV after commissioning of the second PU.
3.2.5. Starting Equipment IC must provide: transportation ILV in a horizontal position with the LC and SC to RKN (if necessary) back. installation, retention, and parking space rocket at PU, preparation and launch of ILV in accordance with the ID of the ILV. dock with ground equipment airborne communications disconnection RKN and their start-up or before the start of ILV; unstressed ILV treatment with CP in accordance with the characteristics of the flight of RKN at the initial part of the standard and nonstandard paths given in the ID of ILV; nezapravlennoy parking space rocket launchers for up to 7 days.
3.2.6. Filling Equipment IC should provide the necessary number of refills blocks propellant rocket with the parameters defined in the ID of the ILV.
3.2.7. Gas supply equipment shall provide IC production, storage and delivery of compressed gases in pH (in accordance with the parameters defined in the ID of the ILV and consumers NC.
3.2.8. thermostatting equipment must be capable of providing a fluid compartments in the ILV with the given parameters of flow rate, temperature, purity and moisture content specified in the ID of the ILV.
3.2.9. Equipment control, power supply and control IC must provide: management of technological operations in the process of preparing and launching space rocket; conduct the final operations and carry out works after the start of RKN associated with reduction complex to its original state; electricity consumers IC voltage three-phase alternating current of 380/220 kV and 10 kV (if necessary), 50 Hz to 1 category of reliability in accordance with the EMP (Edition 7), including a special group of users on the system of guaranteed power supplies. quality standards of electricity must comply with GOST 13109-97; electricity consumers IC DC in accordance with their requirements; power supply voltage AC 208/120 V, frequency 60 Hz and 380/220 V, 50-60 Hz for the equipment of a foreign the customer; measurement parameters of functioning equipment Insurance (including gas-dynamic and acoustic parameters during startup); television monitor and RKN-tech equipment to the registration of the television media during the entire period during which RKN at LC.
3.2.10. The equipment should launch pad ensure portability starting ILV for 24 hours with a drain and refill without refilling storage IC (when moving start ILV is to CP in a vertical position.)
3.2.11. Equipment IC must ensure stockpiles propellant components and compressed gases, enough to make one cycle of RKN for launch, including: park "dry" ILV, ILV fueling MCT park tucked ILV, discharge from the tanks CRT ILV, ILV parking nezapravlennoy after discharge CMT, refilling and start ILV, a second sink in the event of cancellation of start-up.
3.2. 12. Equipment Insurance shall provide for the collection of industrial wastes fuel used to fuel launch vehicle.
3.2.13. Equipment Security IC must provide: fire and explosion safety during all activities, as well as environmental and industrial safety. presence of control, prevention, containment and prevention of fire and emergency situations at the SC. 3.2.14. PU SC must ensure the withdrawal of gas jets control pH and acceptable levels of gas dynamics, shock wave, thermal and acoustic loads on the ILV and Equipment Insurance. Admissible levels of loads on the ILV must be specified in The ID of the ILV.
3.2.15. Equipment IC must provide training to launch space rocket at any time of day and year according to the climatic conditions specified in the ID of the ILV. 3.2.16. The IC must be ensured synchronization of processing equipment, incoming in its composition, in relation to the same time. 02/03/17. Equipment IC must ensure that the necessary work for the abolition of start-up, drain the fuel components of the tanks RKN and relieving pressure in gas cylinders ILV, ILV withdrawal from CP and transporting it to the TC.
3.2.18. Buildings Insurance must provide accommodation and the necessary conditions for the functioning of the equipment Insurance (systems, components and assemblies), including spare parts, taking into account the requirements of the equipment requirements and operating personnel SC.
3.2.19. Technical systems must operate the equipment Insurance, safety and livelihoods of the staff, as well as protection from external climatic conditions.
3.2.20. shall be lightning ILV installed on PU and lightning protection facilities of the complex. Buildings Insurance must have the line terminal.
3.2.21. In the course of EP leading developer of SC (with the assistance of the project organization) should be developed master plan scheme SC, as well as conducted and linkage of process equipment with facilities SK.
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On trouvera un appel d'offre similaire pour le pad soyouz 2 à cette même adresse.