Multipurpose Fregat
Base Fregat upper stage marked the start of the whole family of highly effective upper stages, which were produced and are produced on its base. Application on the Fregat upper stage of additional fuel tanks and jettisonable tanks unit (Fregat-MT and Fregat-SB) made it possible to significantly increase the mass of loaded fuel and thereby increase the efficiency of the upper stage.
The basis of the structural-layout scheme of the Fregat upper stage is a block of tanks built according to a monoblock carrier scheme. It has a torospheric configuration, consisting of six spherical containers welded together, separated by spherical bottoms. Four of them are oxidizer and fuel tanks, two tanks are compartments for on-board instruments and equipment (one of them is sealed).
One of the containers (sealed) contains a monoblock of the control system including satellite navigation equipment and ventilators of thermal control system, another one (not sealed) contains a small instrument compartment, service units, as well as high pressure spherical tanks of sustainer propulsion system and propulsion system of attitude control system (ACS).
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Features of "Fregat"
- autonomous, i.e. provides the whole process of payload injection without interference front he ground;
- Fregat operation logic envisages a way out from possible non-nominal situations;
- upper stage provides almost the absolute accuracy of spacecraft injection into target orbits;
- for the first time in Russia satellite navigation equipment, operating from GLONASS and GPS navigation systems was used in the control loop, thereby significantly increasing the accuracy of spacecraft injection into target orbits;
- possibility of multiple switching on of sustainer propulsion system with the aim of ensuring of optimal injection;
- Fregat upper stage is fueled with fuel components before installation on the launch site which makes it universal with respect to any launch vehicles;
- long active life time длительное время (up to 2 days);
- possibility to ensure launches from 4 cosmodromes: Baikonur, Vostochny, Plesetsk and Kourou Guiana Space Center (French Guiana).
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Systems included in the "Fregat"
- propulsion system consisting of: sustainer propulsion system, stabilization, orientation and launch ensuring propulsion system;
- control system;
- telemetry system;
- transmitting device;
- antenna feeder systems;
- chemical current sources;
- thermal control system (TCS);
- temperature and pressure control system;
- radio-range-finder;
- service units.
Main characteristics
Parameters |
Fregat
|
Fregat-MT
|
Fregat-SB
|
---|---|---|---|
Initial mass with maximum fueling, kg | 6235 | 7640 | 11680 |
Final mass, kg | 945 | 1035 | 1080 |
Dimensions: height/diame ter, mm | 1875/3440 | 1945/3800 | 2435/3875 |
Fuel components: oxidizer/fuel | nitrogen tetroxide / unsymmetrical dimethylhydrazine | nitrogen tetroxide / unsymmetrical dimethylhydrazine | nitrogen tetroxide / unsymmetrical dimethylhydrazine |
Maximum operational fuel reserve/full fueling, kg | 5235/5307 | 6550/6650 | 10140/10330 |
Sustainer propulsion system thrust: BT/MT mode, kgf. | 2030±100/1420±150 | 2030±100/1420±150 | 2030±100/1420±15 |
Specific impulse: BT/MT mode, f | 333,2/320 | 333,2/320 | 333,2/320 |
Maximum switch on number of sustainer engine | 7 | 7 | 7 |