CHAPTER 3: Weapons and Equipment
Section V: Anti-Tank
AT Grenade launcher |
|||||
| Projectile | PG-7 |
PG-7M |
PG-VR |
PG-VL |
OG-7/7V |
| Range, moving/stationary tgt | 300/500 |
||||
| velocity (mps) | |||||
| armor penetration (mm) | 330 |
330 |
>750 |
>PG-7M <PG-VR |
|
| warhead type | HEAT |
HEAT |
tandem HEAT |
HEAT |
HE-Frag |
| warhead caliber (mm) | 85 |
72 |
105 |
93 |
|
| length (mm) | |||||
| weight (kg) | 2.2 |
2 |
4.5 |
2.6 |
|
| rate of fire (rpm) | 6 |
6 |
6 |
6 |
6 |
| unit of fire | 5 |
5 |
5 |
5 |
5 |
| crew | |||||
| Launcher | |||||
| tube caliber (mm) | 40 |
40 |
40 |
40 |
40 |
| length (mm) | 953 |
953 |
953 |
953 |
953 |
| weight (kg) | 7.9 |
7.9 |
7.9 |
7.9 |
7.9 |
| AT Grenade launcher | RPG-16D | RPG-18 | RPG-22 | RPO-A |
| Projectile | PG-16 |
|||
| Range, moving/stationary tgt | 500/800 |
?/200 |
?/250 |
200 DF 1000 IDF |
| velocity (mps) | 130 |
115 |
||
| armor penetration (mm) | 375 |
360 |
390 |
|
| warhead type | HEAT |
HEAT |
HEAT |
FAE |
| warhead caliber (mm) | 58.3 |
|||
| length (mm) | 600 |
670 |
||
| weight (kg) | 3 |
1.4 |
1.8 |
2.3 |
| rate of fire (rpm) | 6 |
NA |
NA |
2 |
| unit of fire | ||||
| crew | 2 |
1 |
||
| Launcher | ||||
| tube caliber (mm) | 58.3 |
64 |
73 |
93 |
| length (mm) | 1100 |
1050 |
850 |
920 |
| weight (kg) | 10.3 |
2.7 |
3 |
3.5 |
AT Guns & Rifles |
||||
| range, HEAT (m) | 5,955 |
1,000 |
500 |
|
| HEAT-RA | 250 |
|||
| HVAPFSDS | 3,000 |
NA |
||
| APDS | 2,100 |
NA |
||
| ATGM | 5,000 |
5000 (AT-11) |
NA |
|
| HE | 500 |
|||
| indirect fire | 8,200 |
12,200 |
1,000 HE, 1300 m smoke, 2300 m illum |
|
| armor penetration (mm) | 400 HEAT, 250 APDSFS, 700 AT-10 |
400 HEAT, 570 APDS, 770 AT-11a, 1050 AT-11b |
400 |
500 HEAT, 900 HEAT-RA |
| rate of fire, maximum (rpm) | 8 |
6 |
||
| sustained | 14 |
100 rph |
6 |
|
| fire control | May have automated fire control with thermal sights. |
DVO, II, thermal |
DVO, II |
3x DVO |
| ammunition types | HE-Frag, HEAT-FS, APFSDS, AT-10 |
HE-Frag, HEAT-FS, APFSDS, ATGM |
HEAT, HE-RAP, AP AT hollow charge |
HEAT, HEAT-RA, illumination, smoke, HEDP, HE |
| elevation (degrees) | -6 TO 20 |
-6 to +25 |
-3 to 7 |
|
| traverse (degrees) | 54 |
-360 |
30 |
|
| emplace/displace time (min) | 2 TO 3 |
0.5 |
||
| crew | 6 |
7 |
3 or 4 |
|
| weight (kg) | 3,050 |
6,500 |
60 |
|
| dimensions L xW x H (m) | 2.11 x 0.99 x 0.8 |
1.065 long |
Antitank Guided Missiles (ATGM) |
AT-3c SAGGER 9K11 Malyutka |
AT-4a/b SPIGOT 9K111/9K111M Fagot/Faktoriya |
AT-5 a/b SPANDREL 9K133/9K133m Konkurs/Konkurs-M |
AT-6 a/b/c SPIRAL 9K114 Shturm |
| range(m) | 500-3000 |
70-2000/ 75-3500 |
70-4000/ 75-4000 |
400-5000/ 400-5000/ 400-6000 |
| flight time to max. range (sec) | 23-26 |
11/19.5 |
19 |
13.3/ 16/ 18.6 |
| penetration (RHA/behind ERA mm) | 9M14M: 400, 9M14P: 460, 9M14P1: 520, 9M14-2: 800 |
AT-4A: 600, AT-4b: 650 |
AT-5a: 650, AT-5b: 925/800 |
700/ 950/ 950 |
| guidance & command link | wire MCLOS, 9M14-2: wire SACLOS |
wire SACLOS |
wire SACLOS |
RF SACLOS |
| launching platform | tripod (suitcase), 9P133 (BRDM-2), 9P122 (BRDM-2), BMP-1, BMD-1, BOV-1, M-80, Mi-2 HOPLITE, Mi-8 HIP, Gazelle |
9P135 tripod, BMP-1P, BMP-2, BMD-1P,BMD-2, BTR-RD, 9P148 (MT-LB), LuAZ-967 Lt all-terrain vehicle |
BMD-1/2/3, 9P135M tripod, BMP-1P/2, UAZ-469, BTR-D, 9P148 (MT-LB) |
9P149 (MT-LB), Mi-24 HIND, Ka-29 HELIX |
| weight, preflight (kg) | 11.3-12.5 |
AT-4a: 7.4 |
31.4/ 33.5/ ? |
|
| length (mm) | 860-925 |
863/865 |
AT-5a: 1150 |
1625/ 1745/ 1625 |
| diameter (mm) | 125 |
119/120 |
AT-5a: 135 |
130 |
| fin span (mm) | 370 |
354/369 |
AT-5a: 468 |
360 |
| warheads | HEAT, 9M14-2: tandem HEAT |
HEAT |
HEAT/ tandem HEAT |
HEAT or FAE |
| remarks | The AT-3 continued to be improved and proliferated worldwide. The (m14-2 missile is effective against reactive armor. |
Thermal sight detection range is 3600 m, identification at 2000 m. |
Thermal sight detection range is 3600 m, identification at 2000 m. |
FAE range 400-5000 m. |
Antitank Guided Missiles (ATGM) |
AT-7 SAXHORN 9K115 Metis |
AT-8 SONGSTER 9K112 Kobra |
AT-9 9K120 Ataka |
AT-10 STABBER 9K116-1/9K116 Bastion/Kastet |
| range(m) | 40-1000 |
100-4000 |
400-6000 |
100-5000 |
| flight time to max. range (sec) | 6 |
10 |
14.5 |
15 |
| penetration (RHA/behind ERA mm) | 500 |
800 |
1000/800 |
660 |
| guidance & command link | wire SACLOS |
RF (30GHz) SACLOS |
laser beam rider SACLOS |
|
| launching platform | 9P151 firing post |
T-64B/B1/B1K, T-80B/BVK |
9P149 (MT-LB), Mi-24 HIND, Mi-35 HIND, Ka-29 HELIX, Mi-28 HAVOC |
MT-12, BMP-3, T-55AMB, T-55AM2, T-55AMV |
| weight, preflight (kg) | 5.5 |
24.5 |
||
| length (mm) | 740 |
1047 |
1047 |
|
| diameter (mm) | 94 |
100 |
130 |
100 |
| fin span (mm) | 300 |
257 |
750 |
257 |
| warheads | HEAT |
HEAT |
tandem HEAT, blast, FAE, anti-helicopter |
HEAT |
| remarks | Thermal sight detection range is 3200 m, identification at 1600 m. Emplace/displace times are 12/20 seconds. |
Fired through the main gun tube. |
Fired through the main gun tube. Off BMP-3 range is 100-4000 m, but it can fire on the move. |
Antitank Guided Missiles (ATGM) |
AT-11a/b SNIPER 9K119/9K119M Svir/Invar |
AT-12 STABBER 9K116-2 Sheksna |
AT-13 9K115-2 Metis-M |
AT-14 Kornet |
| range(m) | 100-5000 |
100-5000 |
80-1500 |
100-5500 |
| flight time to max. range (sec) | 15 |
12 to 4000 m |
8.4 |
22 |
| penetration (RHA/behind ERA mm) | 770 AT-11a, 1050 at-11b |
800 |
1000/800 |
1200/980 |
| guidance & command link | laser beam rider SACLOS |
laser beam rider SACLOS |
wire SACLOS |
laser beam rider SACLOS |
| launching platform | T-72B, T-72S, T-72V, T-80U, T-72UD,T-90, 2A45M AT gun |
T-62M |
9p151 tripod, UAZ-459 |
tripod, UAZ-469 "jeep", APC |
| weight, preflight (kg) | 28/24.3 |
18.4 |
13 |
27 |
| length (mm) | 700 |
1084 |
910 |
1200 |
| diameter (mm) | 125 |
115 |
127 |
152 |
| fin span (mm) | 160 |
255 |
400 |
|
| warheads | HEAT/tandem HEAT |
HEAT |
tandem HEAT, FAE |
tandem HEAT, FAE |
| remarks | Fired through the main gun tube. T-72 variants have a 4000-m maximum range. |
Fired from the halt through main gun tube. |
FAE has greater power than 152-mm artillery round. |
Thermal sight range is 4000-m detection & 3500 m identification. Maximum altitude of engaged helicopters is 3000 m. |
Antitank Guided Missiles (ATGM) |
AT-16 9K121 VIKhR |
Milan (FR) 1/2/2T/3 |
Tow (US) |
HOT (FR/GE) |
| range(m) | 1000-10,000 |
20-2000 |
3750/3750/ |
75-4000 |
| flight time to max. range (sec) | 23 |
12.5 |
2a: 20, 2b: 21 |
16.5 |
| penetration (RHA/behind ERA mm) | 1050/900 |
600/1060/1200/1200 |
500, ITOW:800, 2:920 2a:1000 |
850, 2:950 |
| guidance & command link | laser beam rider SACLOS, lock on before launch |
1&2: SACLOS wire SACLOS IR |
SACLOS wire |
SACLOS wire |
| launching platform | Ka-50 HOKUM, Su-25 FROGFOOT |
tripod, compact turret, Marder 1A3 |
tripod, M113, Bradley IFV, M901a2, HMMWV, LAV-AT, UH-1J |
tripod, vehicles, helicopter |
| weight, preflight (kg) | 45 |
1&2: 6.7 |
1&2: 28.1 |
1: 23 2:23.5 |
| length (mm) | 1500 |
|||
| diameter (mm) | 130 |
|||
| fin span (mm) | ||||
| warheads | tandem HEAT |
|||
| remarks | Maximum airborne-target speed 800 kph. |
Milan 3 medium range ATGM has IR command link resistant to jammikng and tandem warhead. |
Tow 2b is fly over, shoot down top attack with self-forming penetrater. 2nd gen FLIR. |
HOT 3 long range ATGM has a tandem warhead, bispectral day/night sights and maybe mounted post, vehicles or helicopters |
| Any changes from the 1998 OPFOR Battle
Book are depicted in GREEN printing. Last updated on 13 April, 1999 For any comments, additions, deletions, or modifications for this Battle Book contact LTC Bill Bryan. |