9K34 Strela-3
From Wikipedia, the free encyclopedia
The 9K34 Strela-3 (Russian: 9К34 «Стрела-3»; English: arrow) man-portable air defence missile system (MANPADS) was developed in the Soviet Union as a response to the poor performance of the earlier 9K32 Strela 2 (SA-7 Grail) system. "9K34" is its GRAU designation. And its NATO reporting name is SA-14 Gremlin. The missile was largely based on the earlier Strela 2, and thus development proceeded rapidly. The new weapon was accepted to service in the Soviet Army in January 1974.
The most significant change was the introduction of an all-new infra-red homing seeker head. The new seeker worked on FM modulation (con-scan) principle, which is less vulnerable to jamming and decoy flares than the earlier AM (spin-scan) seekers, which were easily fooled by flares and even the most primitive infrared jammers. Most importantly, the new seeker also introduced detector element cooling in the form of a pressurized nitrogen bottle attached to the launcher.
The effect of cooling was to expand the seeker's lead sulphide detector element's sensitivity range to longer wavelengths (slightly over 4 µm as opposed to 2.8 µm of uncooled PbS elements). In practice this made possible the tracking of cooler targets over longer ranges, and enabled forward-hemisphere engagement of jets under favourable circumstances.
The seeker also had better tracking rate, enabling the missile to track maneuvering or fast and approaching targets.
Strela-3 missiles have been exported to over 30 countries.
The original Strela-3 missile was the 9M36. The follow-on to the Strela-3 was Igla.
The naval version of this missile has the NATO reporting name of SA-N-8.
[edit] Comparison chart
| System | 9K32M Strela-2M (missile: 9M32M) | 9K34 Strela-3 (missile: 9M36) | FIM-43C Redeye |
| Service entry | 1970 | 1974 | 1968 |
| Mass, full system, ready to shoot | 15 kg | 16 kg | 13.3 kg |
| Weight, missile | 9.8 kg | 10.3 kg | 8.3 kg |
| Length | 1.44 m | 1.47 m | 1.40 m |
| Warhead | 1.17 kg (0.39 kg HMX) directed-energy blast fragmentation | 1.17 kg (0.39 kg HMX) directed-energy blast fragmentation. A secondary charge sets off remaining propellant | 1.06 kg M222 (0.36 kg HTA-3) blast fragmentation |
| Seeker type | AM-modulated (spin scan), uncooled PbS detector element (1–2.8 µm sensitivity range). Tail-chase only. | FM-modulated (con scan), nitrogen-cooled PbS detector element (2–4.3 µm sensitivity range). Limited forward hemisphere (all-aspect) capability | AM-modulated, uncooled PbS detector element. Tail-chase only. |
| Maximum range | 4200 m | 4100 m | 4500 m |
| Speed | 500 m/s | 470 m/s | 580 m/s |
| Target's maximum speed, approaching/receding | 150/260 m/s | 260/310 m/s | –/225 m/s |
| Engagement altitude | 0.05-2.3 km | 0.03-3 km | 0.05-2.7 km |
| Russian and former Soviet surface-to-air missiles |
|
The SA designation sequence: |
| List of Russian and former Soviet missiles Missiles |
