S-25
SA-1 GUILD
| Specifications | |
|---|---|
|
DOI |
|
Type | 217M Surface-to-air missile |
| Performance: | |
| Altitude Range defeat: |
C-25 - 3 000 - 25 000 m C-25M - 1 500 - 25 000 meters |
| maximum range of the defeat: |
S-25 - 35 000 m C-25M - 40, 000 meters |
| Maximum Speed: |
C-25 - 347 m / s C-25M - 555 m / s |
| Kill Radius | |
| Reload time (min) | |
| Associated radars | |
| Housing: | |
| Caliber | 650 mm; |
| Theoretical length (without gas rudders and tubes LDPE) | 12216 mm; |
| Overall length (with gas rudders and tube LDPE) | 12 856 mm; |
| Overall length (with safety covers) | 12 962 mm; |
| Wings: | |
| The scope of the theoretical | 2655 mm; |
| Swing position (with winglets) | 2735 mm; |
| Mean aerodynamic chord | 2038 mm; |
| The scope of the aileron | 650 mm; |
| Deviation angle - aileron | ± 20 ° ± 1 °; |
| Air rudders: | |
| The scope of the theoretical rudder | 1416 mm; |
| Swing position (with winglets) | 1426 mm; |
| Mean aerodynamic chord rotating part | 406 mm; |
| The angle of deviation | ± 16 ° ± 30 '; |
| Stabilizers: | |
| The scope of the theoretical | 1030 mm; |
| stabilizing overall scope: | |
| Horizontal (with fairing) | 1100 mm; |
| Vertical (with winglets) | 1048 mm; |
| Gas rudders: | |
| The scope of helm | 91 mm; |
| Distance from the axis of rotation of the wheel to the edge of the nozzle | 80 mm; |
| The angle of deviation | ± 18 ° ± 1 °; |
| Mass characteristics: | |
| Weight fully equipped and tucked missiles with gas rudders | 3975 kg; |
| Curb weight and unmade missiles without gas rudders | 1360 ± 50 kg; |
| The mass of filling (fuel and air) | 2610 kg; |
| Warhead weight | 280 kg; |
| The mass of the discharged gas rudders parts | 4.18 kg; |
| The mass of the oxidizer tank O | 1919.8 kg; |
| The mass of the oxidant in the pipeline | 28.48 kg; |
| The mass of fuel in the tank T | 627.8 kg; |
| The mass of fuel in the pipeline | 7.73 kg; |
| The mass of air in the system control | 14.9 kg; |
| The mass of air in the system AP | 10.3 kg; |
| The mass of powder for TNA | 1 kg; |
| The mass of the silica gel | 2 kg; |
| The warranty period and service life | Shelf life is 5 years missiles under the following storage conditions: |
| In heated storage | up to 5 years; |
| In unheated storage | up to 2 years; |
| Air cylinders with tucked | up to 2.5 years; |
| A seasoned tank T | 2.5 years; |
| About a seasoned tank | up to 2 years; |
| In the open air under natural conditions | up to 1 year. Warranty service life of the autopilot AP-25 radio controlled fuses E-802M-P devices System-301-C converter and the TP-900C-2 is not less than 110 hours. |
| Transportation missiles during the warranty period of validity permitted missiles for distances: | |
| Rail | 4000 km; |
| Motor vehicles on highways at speeds up to 40 km / h | 1000 km; |
| Including an improved dirt roads at speeds up to 20 km / h | 300 km. |
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