CALT A-100
Notes: The A-100
is a derivative of the WS-1, designed to replace the WS-1 and supplement the
WS-1B. The A-100 is a GMLRS, firing
guided or unguided rockets. The
A-100 is further a derivative of the Russian Smerch 9K58 launcher, but using a
Chinese truck chassis instead of a Russian truck chassis. CALT (China Academy of
Launch Vehicle technology), is a design bureau more associated with spacecraft
boosters and ballistic missiles; this is their attempt to break into the
military rocket market, and it seems to be successful so far, as the PLA seems
to be impressed with the system. Other users include Pakistan and Tanzania. (It
should be noted that the A-100 turned out very different from its Russian
counterpart; for example, Smerch rockets will not fit into an A-100 launcher,
despite being the same caliber.) These vehicles are assigned at Division, Corps,
and Army levels and are expected to have a lot of speed, and they don’t.
A-100
The rockets and
missiles fired from the A-100 are 300mm, and launch anything from conventional
warheads with a variety of warheads to the PLA’s preferred rounds, missiles with
several types of warheads. (Reportedly, the PLA’s favorite warhead for the A-100
is a SADARM-type warhead.) The
launcher has ten tubes (though early development designs used only six tubes);
the launchers are arranged with four tubes on top, and six on the bottom row.
The guided version uses a simple motion detector with a computer that
corrects for drift. This computer
also triggers warheads such as DPICM and SADARM to that they detonate at the
optimum altitude to achieve the best spread.
The chassis of
the launch vehicle is based on the Tai’an TAS5380 8x8 heavy truck.
The TAS5380 was designed specifically to carry and act as a TEL for large
missiles and rockets. The engine is
a Deutz turbocharged diesel with 517 horsepower, and coupled to automatic
transmission. The chassis has a
central tire pressure system and puncture-resistant run-flat tires.
The cab has air conditioning, heating, and is NBC-Sealed. Behind the cab
is a sealed section for the vehicle’s electronics, radios, land navigation
system, and vehicle state system.
The cab is designed for five people, but has a crew of only three, so there is a
decent amount of room, even with the gunner’s fire control equipment, for
personal equipment and even a 30-liter drinking water tank.
A-100E
This is a
version with modifications specifically for Pakistan.
It is built in Pakistan under license
and most of the modifications are to suit local manufacturing methods.
It uses a truck similar to the TAS5380, the TAS4500; the main difference
is that the TAS4500 is a newer design.
The Pakistanis acquired the A-100E specifically to counter India’s
purchase of the 9A52-2T Smerch. The
A-100E has a slightly upgraded guidance system, and the on-missile computer is
tweaked to reflect the Pakistani Army’s preference for a lower burst altitude
for DPICM and SADARM warheads.
A-200
This fs for the
most part the same as the A-100, but uses inertial positioning as its main
guidance, with updates on position done by GPS several times during flight.
The fire control equipment is updated with a GPS receiver to give the
missiles an initial fix. The
missiles are also differently positioned on the launcher; there are three
missiles on the top and bottom, with two in between.
The missiles used with the A-200 are further modified with forward
control surfaces that are not present on A-100 rockets.
This system is available on the arms market, but has had no takers as of
yet.
A-300
The A-300
uses simultaneous GPS and inertial guidance, making it very accurate.
It also has an extended range of 290 kilometers, as opposed to the 100
kilometers of other versions. Fire control is appropriately modified. It is
otherwise the same as the A-200.
AR1A
This launcher
system was developed from the A-100 when the PLA chose not to use that vehicle.
The PLA, unfortunately, also chose to pass on the AR1A; however, Armenia
is reportedly using the AR1A. The
TEL is loaded with two 5-round sections, each of which has two rockets on the
top and bottom and one in the middle. It’s are long range for MLRS rockets,
having a range of 130 kilometers.
The TEL is based on a Wanshan WS2400, which, despite being about a meter longer,
is about the same design and same engine power as the other launchers in this
series.
AR3
Perhaps one of
the most powerful GMLRSs in the world, the AR3 fires 370mm guided missiles as a
primary munition, though it can also mount the AR1A’s rocket pack.
The missiles are guided by inertial navigation with GPS updates.
The AR3 uses the same TEL as the AR1A.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological* |
A-100 |
$911,150 |
D, A |
710 kg |
43 tons |
3 |
32 |
2nd Gen FLIR, 2nd Gen Image Intensification (G),
2xCCD Cameras (G, C) |
Shielded |
A-100E |
$921,150 |
D, A |
735 kg |
43 tons |
3 |
32 |
2nd Gen FLIR, 2nd Gen Image Intensification (G),
2xCCD Cameras (G, C) |
Shielded |
A-200 |
$934,483 |
D, A |
735 kg |
42 tons |
3 |
33 |
2nd Gen FLIR, 2nd Gen Image Intensification (G),
2xCCD Cameras (G, C) |
Shielded |
A-300 |
$987,817 |
D, A |
740 kg |
42 tons |
3 |
33 |
2nd Gen FLIR, 2nd Gen Image Intensification (G),
2xCCD Cameras (G, C) |
Shielded |
AR1A |
$828,350 |
D, A |
750 kg |
43.5 tons |
4 |
34 |
FLIR, Image Intensification (G), 2xCCD Cameras |
Shielded |
AR3 |
$1,244,453 |
D, A |
788 kg |
44 tons |
4 |
37 |
2nd Gen FLIR, 2nd Gen Image Intensification (G),
2xCCD Cameras (G, C) |
Shielded |
Vehicle |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
A-100/100E |
110/55 |
30/15 |
825 |
196 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
A-200/300 |
112/56 |
31/16 |
825 |
196 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
AR1A |
109/55 |
30/15 |
825 |
196 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
AR3 |
109/55 |
30/15 |
825 |
196 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
A-100 |
+2 |
None |
10-round 300mm Missile Launcher |
10x300mm Missiles |
A-100E |
+2 |
None |
10-round 300mm Missile Launcher |
10x300mm Missiles |
A-200 |
+3 |
None |
8-round 300mm Missile Launcher |
8x300mm Missiles |
A-300 |
+4 |
None |
8-round 300mm Missile Launcher |
8x300mm LR Missiles |
AR1A |
+2 |
None |
10-round 300mm Rocket Launcher |
10x300mm LR Rockets |
AR3 |
+4 |
None |
8-round 370mm Missile Launcher |
8x370mm Missiles |
Norinco Type 70 MRL
Notes:
This is the same rocket launcher as mounted on the Type 82 130mm MRL,
this time mounted on the chassis of a YW531 APC (Type 63) on an
electrically-powered turret. The
passenger area of the YW-531 is taken up with the turret for the MRL, fire
control equipment, communications gear, an extra rocket pack, and the crew. The
driver is on the front left; he has a night vision block for his position, but
this does not give him a wide field of view.
The Type 70 MRL is believed to have been replaced by an MRL based on the
Type 89 APC, but the Type 70s are still in reserve duties.
The chassis
otherwise remains similar to the YW531, with four roadwheels per side, a drive
sprocket, and an idler wheel at the rear.
Engine is the same KHD BF8L 413F with 320 horsepower and manual
transmission.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$131,339 |
D, A |
500 kg |
14 tons |
6 |
12 |
Passive IR (D) |
Enclosed |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
159/111 |
44/31/4 |
450 |
95 |
Trtd |
T4 |
TF2 TS2
TR2 HF3
HS2 HR2 |
Fire Control |
Stabilization |
Armament |
Ammunition |
None |
None |
19-round 130mm Multiple Rocket Launcher, DShK (C) |
38x130mm Rockets, 600x12.7mm |
Nanjing Type 81 107mm MRL
Notes:
In the early 1970s, China developed a towed 107mm MRL for export for use
by light mobile forces, designed to be towed by a light vehicle and in general
very light in weight and size. The Type 81 uses this MRL, the Type 63, mounted
on the back of a Nanjing NJ-230 4x4 light truck, with a manual transmission and
a 120-horsepower engine. The truck
chassis is mostly unmodified from the standard truck, and simply has the MRL
mounted on a manually-turning pedestal with stops to lock the MRL down when
firing position is reached, and only the most rudimentary of aiming mechanisms.
Because of the inaccuracy of a barrage fired by the Type 81, all scatter
distances double. The cab is
enlarged for the crew, but firing mechanisms consist of simply a few switches
and safeties. About half of the
cargo area is taken up with the MRL, but there is an area available for crew
equipment, spare tire, and tools.
Many Type 81s are further modified with a metal or wood box on the front bumper
and hood for carrying extra rounds.
This MRL is often mistakenly referred to as the Type 63 MRL, though the Type 63
designation actually only applies to the MRL and not the entire system. Though
the Type 81 is not used by the PLA, it is used Iran (where it is known as the
Haseb), Sudan (called the Taka), South Africa (called the RO 107), and on the
North Korean VTT-323 armored vehicle chassis.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$49,661 |
G, A |
400 kg |
3.71 tons |
4 |
4 |
Headlights |
Open |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
232/117 |
65/33 |
105 |
53 |
Trtd |
W(2) |
TF1 TS1
TR1 HF1
HS1 HR1 |
Fire Control |
Stabilization |
Armament |
Ammunition |
None |
None |
12-round 107mm Rocket Launcher |
24x107mm Rockets |
Norinco Type 81 122mm MRL
Notes: This
variant of the Soviet BM-21 Grad SPMRL is produced primarily for the PLA.
In fact, many “BM-21s” spotted worldwide are in fact Type 81s, most
notably those used by Vietnam in their invasion of the South. The Type 81 is
mounted on the rear of a Shaanxi SX250, which is a modified version of the
Hanyang CQ260 6x6 heavy truck chassis (which is itself a modified form of the
French Berliet GBU 15). This
chassis has a 320-horsepower engine and a manual transmission. The rockets are
on a turntable on the rear of the truck chassis and can be traversed left 70
degrees and right 180 degrees, with
a depression of 0 degrees and an elevation of +55 degrees..
The vehicle is capable of acting as its own FDC, but medium and
long-range scatter is doubled, despite a simple ballistic computer and inertial
navigation. The truck has an enlarged, lightly-armored cab primarily meant to
insulate the crew from the exhaust of the rockets. The MRL may be fired in
manual (1 shot at a time), semiautomatic (20-round ripple) or automatic
(40-round full ripple) modes. The enlarged cab contains positions for the
driver, commander, gunner, and assistant gunner; a further three crewmembers,
who are loaders, are carried on an accompanying truck. The MRL fills almost the
entire cargo area, except for a small space behind the cab for a spare tire, a
seat for part of the crew, and crew equipment.
This system was replaced in production by the Type 90 MRL, but remains in
service with many Chinese units.
A variant, the
SR-4 uses two pods of 20 instead of a single pod of 40.
It is otherwise, for game purposes, the same as the Type 81, except that
the SR-4 may be fired with only one pod in place.
The Type 83 MRL
is a variant of this launcher carrying four rows of six rockets instead of four
rows of ten, mounted on a smaller DongFeng
CA-30 truck. Though it was
primarily designed for export, the PLA has discovered that the lighter vehicle
is useful in light motorized units.
The CA-30 base chassis is much lighter than that of the Type 81, and develops
only 96 horsepower, coupled to a manual transmission.
The cab is lightly armored, more to protect the crew against the rocket
exhaust than anything else. The cab is not enlarged, but there is room for only
three in it; the rest of the room is taken up by a space for personal gear and
the fire control board and electronics.
(Another three crew members ride on the trucks that carry reload
rockets.) The rear area of the
chassis carries the launcher (which takes up most of the room), a spare tire,
and some tools and other ancillary items.
The Type 83 has a primary role in the PLA of sowing minefields from
FASCAM rounds, but it is perfectly capable of firing other 122mm rounds.
The Type 90 is
the same launcher mounted on a Tiema SC2030 6x6 truck chassis. This chassis is
longer and wider and is able to carry an additional rocket pack in front of the
mounted pack, along with a light crane to lift the expended pack off and the
fresh pack onto the pedestal. Three
people, however, are required for this operation. Reloading takes 3 minutes. The
truck has an engine rated at 322 horsepower, with an automatic transmission.
The cab is lightly-armored, NBC sealed, and has a air conditioning unit
on the roof of the cab which is NBC filtered. The cab is enlarged to give room
for the fire control equipment, radios, and a space for personal gear. Fire
control computers are digital, and as the Type 90 has the capability to depress
to zero degrees, a laser rangefinder is available for direct-fire shots.
Normal firing is done with inertial navigation and a mapping module,
along with a small computer module with maps of the potential battle area (and
this module is able to be updated). The vehicle has automatic laying and
reloading systems that allow the MRL to fire accurately without the assistance
of an FDC if the target location is known.
The actual crew of the vehicle is six, but the other three crewmembers
(usually loaders) ride in resupply vehicles.
The Type 90A is
an upgrade of the Type 90, particularly in the chassis, which is a Tienna XC2200
truck with a 350-horsepower engine, automatic transmission, an automatic fire
detection and suppression system for the engine and transmission, and run-flat,
puncture-resistant tires. In
addition, the fire control suite is updated, with better computers and
equipment, in addition to the inertial navigation and mapping suite of the Type
90. A group of up to six Type 90As
may be controlled from one location by way of wires.
This also allows a command vehicle in a battery to control the entire
battery. On the roof of the cab is
telescopic observation equipment and night vision gear, on a swivel mount.
The Type 90B is
an upgrade of the Type 90A; the launcher is mounted on a somewhat larger,
somewhat more powerful Beifang Benchi 2629 6x6 heavy truck.
As with other MRLs of this series, the cab is enlarged and lightly
armored, and has an NBC overpressure system and an NBC-filtered air conditioning
system, as well as a small mast with visual augmentations. The chassis has
automatic transmission, an ignition pre-heater, and a 377-horsepower
turbocharged diesel engine. The 6x6
suspension has puncture-resistant and run-flat tires. The primary update in the
Type 90B system is actually in the accompanying vehicles, which include several
more Beifang trucks for ammo resupply and other gear, a pair of WZ551
reconnaissance vehicles to check out potential firing sites, and a command
vehicle with improved command and fire control systems.
The PR50 is the
latest operational version of the series, with new rocket pods containing 50
rounds, five rows of ten. The
operating cost and maintenance cycle is less than the Type 90B.
The PR50 is capable of firing several types of long-range rockets with
ranges of up to 50 kilometers. The
Chinese name of the PR50 is Sha Chen Bao, which means Sandstorm. The chassis is,
again, slightly larger; though still a 6x6 heavy truck, it is somewhat larger
and more powerful at 392 horsepower.
The PS50 retains the inertial navigation as a backup, but it’s primary
locational tool is GPS. It also has
self-surveying capability.
The SR-5,
introduced at the 2012 Eurosatory but not yet in service, is an unusual variant
that has one pod of 122mm rockets and one pod of 220mm rockets.
The SR-5 is fully computerized and includes a vehicle state computer in
addition to the electronics listed above for earlier variants. The electronics
are modular and can be replaced by more advanced designs in the future. The SR-5
has an advanced fire control suite.
The crane of the SR-5 can lift pods from the ground or trucks and mount them on
the pedestal without intervention from the crew in the cab or loaders (though in
practice, two loaders insure that proper mating takes place). The same fire
control panel and system controls both the 122mm rockets and the 220mm rockets.
The chassis is a Taian heavy 6x6 truck, with the turbocharged diesel
engine providing 517 horsepower.
The rocket pods are similar to two HIMARS pods side-by-side. The 220mm rocket
pod may be replaced with one carrying a C-705 antiship missile, or one King
Dragon 300 missile (similar to the US ATACMS missile). Rocket pods are
factory-loaded and sealed. Due to
the possibility of firing missiles, and the increased electronics, the cab is
greatly enlarged and carries a crew of five.
Other enhanced features are as other vehicles of this series.
The SR-7 is a
light form of the SR-5, with a launcher for only one rocket or missile pod.
The chassis platform is the same as the SR-5, and the electronics are the
same. The launcher can mount one
pod of 20 122mm rockets, six 220mm rockets, one C-705 missile, or one King
Dragon 300 missile. It’s primary
advantage is the increased mobility.
Note that the 220mm rockets fired
by the SR-5 and SR-7 MRLs can also fire a variety of biological agents, as well
as a 1-kiloton nuclear bomb. These
are not covered on this page. The
SR-5 and SR-7 are also capable of firing guided missile-versions of their
rockets, with HE or DPICM warheads.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
Type 81 |
$188,814 |
D, A |
500 kg |
15.2 tons |
4 |
12 |
Headlights |
Enclosed |
Type 83 |
$127,298 |
G, A |
300 kg |
8.7 tons |
3 |
8 |
Headlights |
Enclosed |
Type 90 |
$270,138 |
D, A |
434 kg |
23.6 tons |
3 |
18 |
Headlights |
Shielded* |
Type 90A |
$323,190 |
D, A |
437 kg |
23.9 tons |
3 |
18 |
Thermal Imaging, Image Intensification (G) |
Shielded* |
Type 90B |
$323,429 |
D, A |
442 kg |
24.3 tons |
3 |
18 |
Thermal Imaging, Image Intensification (G) |
Shielded* |
PS50 |
$400,067 |
D, A |
491 kg |
26.73 tons |
3 |
18 |
Thermal Imaging, Image Intensification (G) |
Shielded* |
SR-5 |
$396,142 |
D, A |
454 kg |
27.3 tons |
5 |
18 |
Thermal Imaging, Image Intensification (G) |
Shielded* |
SR-7 |
$349,893 |
D, A |
463 kg |
25.9 tons |
5 |
17 |
Thermal Imaging, Image Intensification (G) |
Shielded* |
Vehicle |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
Type 81 |
164/83 |
46/23 |
400 |
95 |
Trtd |
W(3) |
TF2 TS2
TR2 HF2 HS2
HR2 |
Type 83 |
102/51 |
28/14 |
150 |
42 |
Trtd |
W(2) |
TF2 TS2
TR2 HF2 HS2
HR2 |
Type 90 |
118/59 |
33/17 |
505 |
119 |
Trtd |
W(3) |
TF2 TS2
TR2 HF2 HS2
HR2 |
Type 90A |
124/62 |
34/18 |
534 |
129 |
Trtd |
W(4) |
TF2 TS2
TR2 HF2 HS2
HR2 |
Type 90B |
130/66 |
36/18 |
580 |
140 |
Trtd |
W(4) |
TF2 TS2
TR2 HF2 HS2
HR2 |
PS50 |
124/62 |
34/18 |
596 |
144 |
Trtd |
W(4) |
TF2 TS2
TR2 HF2 HS2
HR2 |
SR-5 |
151/76 |
42/21 |
600 |
191 |
Trtd |
W(4) |
TF2 TS2
TR2 HF2 HS2
HR2 |
SR-7 |
159/80 |
44/23 |
600 |
186 |
Trtd |
W(4) |
TF2 TS2
TR2 HF2 HS2
HR2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
Type 81 |
+1 |
None |
40-round 122mm Rocket Launcher |
40x122mm Rockets |
Type 83 |
+1 |
None |
24-round 122mm Rocket Launcher |
24x122mm Rockets |
Type 90/90A/90B |
+2 |
None |
40-round 122mm Rocket Launcher |
80x122mm Rockets |
PS50 |
+2 |
None |
50-round 122mm Rocket Launcher |
100x122mm Rockets |
SR-5 |
+3 |
None |
20-round 122mm Rocket Launcher, 6-round 220mm Rocket Launcher |
40x122mm Rockets, 12x220mm Rockets |
SR-7 |
+3 |
None |
20-round 122mm Rocket Launcher or 6-round 220mm Rocket Launcher |
40x122mm Rockets or 12x220mm Rockets |
*These vehicles are Shielded only in the cab.
Hanyang Type 82 MRL
Notes:
The Type 82 is a Chinese-built, 30-tube, 130mm multiple rocket launcher
mounted on a modified EQ-2102 6x6 truck for mobility.
It was designed to replace the aging Type 63 130mm MRL, which by the late
1970s was showing its age; in particular, parts for the Type 63 were becoming
increasingly harder to get. The Type 82 itself was replaced shortly thereafter
with the Type 81 122mm MRL, which had a greater variety of warheads available
and better range. However, some
Type 82s are still in service in reserve formations. The Type 82 was normally
employed at the divisional level.
Up to all 30
rockets may be discharged in 15 seconds (three combat rounds).
Reloads are manually loaded into the launcher tubes, but the Type 82
itself also carries 30 reloads in an armored box on front deck, and there are
usually further reloads carried in additional following trucks. The tubes are
arranged in three rows of ten. The
cab is greatly extended and carries the driver, commander, firing crew, and four
reloading crew.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$213,299 |
D, A |
306 kg |
7.5 tons |
8 |
8 |
Headlights |
Open |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
165/83 |
46/23 |
400 |
47 |
Stnd |
W(3) |
HF1 HS1
HR1 |
Fire Control |
Stabilization |
Armament |
Ammunition |
None |
None |
30-round 130mm Rocket Launcher |
60x130mm rockets |
Type 83 273mm MRL
Notes: Also
known as the WM-40, the Type 83 is a multiple rocket launcher based on a Type
60-1 tracked prime mover, with an engine developing 300 horsepower. The MRL is
designed to conduct massive bombardment of enemy positions, but the rockets and
available warheads leave the Type 83’s rockets unable to completely fulfill this
role, though the sheer blast from such large-caliber rockets are bound to cause
great damage. As a result of this and it’s unspectacular off-road performance,
the Type 83 was withdrawn from service in 1988, replaced by 122mm systems. The
load area in this variant is completely taken up with the rocket launch box and
associated equipment, leaving only the cab for the crew.
The cab has the driver, commander, gunner, assistant gunner, and
navigator, as the vehicle is equipped with inertial navigation, self-surveying
capability, digital fire control, and the ability to plot its own firing
coordinates if the target location is known. The launcher has a depression limit
of +5.5 degrees and an elevation limit of +56 degrees, but the turntable allows
deflection of only 10 degrees in either direction from the front. The chassis
has a somewhat-armored cab, with shutters which can be closed (normally done
when firing). The DShK commander's machinegun of the Type 60-1 prime mover is
retained. When the MRL is fired,
two stabilizers are lowered at the rear of the vehicle.
This system was used only by China.
An alternate use
of the Type 83 was to launch target drones to simulate UAVs and low-flying
aircraft in exercises where SHORAD systems are conducting live fire.
Further development of the Type 83 led to the WM-80 MRL, which came into
service in the 1990s.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$357,118 |
D, A |
500 kg |
15.13 tons |
5 |
12 |
Headlights |
Enclosed |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
141/99 |
39/27 |
375 |
111 |
Trtd |
T2 |
TF2 TS2
TR2 HF2
HS2 HR2 |
Fire Control |
Stabilization |
Armament |
Ammunition |
+1 |
None |
4-round 273mm Rocket Launcher, DShK (C) |
4x273mm rockets, 500x12.7mm |
Type 85 MRL
Notes:
Also known as the YW306, this is the same multiple rocket launcher as the
Type 82 MRL, this time mounted on a Type 85 APC chassis.
In this role, the Type 85 does not carry passengers, instead carrying
additional communications and fire control equipment, allowing the MRL to
operate without an FDC. The turret
is removed and replaced with one mounting the MRL.
The Type 85 APC chassis is a large vehicle, allowing for lots of room for
crew, fire control computers and other FC equipment, inertial navigation with
mapping modules, extra radios, ammunition for the commander’s machinegun, and
creature comforts such as NBC Overpressure with vehicular backup, filtered AC,
and a 30-liter drinking-water tank.
Though the Type
85 MRL has a slightly lowered rear deck where the rocket launcher is mounted, it
is otherwise like the Type 85 APC.
Suspension is by torsions bars connecting the roadwheels, and the engine outputs
320 horsepower from a Deutz BF8L 412F 320 horsepower engine coupled to a
semiautomatic transmission.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$180,330 |
D, A |
500 kg |
14.5 tons |
6 |
12 |
Active/Passive IR (D) |
Shielded |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
154/108 |
43/20/4 |
400 |
111 |
Trtd |
T4 |
TF2 TS2
TR2 HF4
HS2 HR2 |
Fire Control |
Stabilization |
Armament |
Ammunition |
None |
None |
30-round 130mm Rocket Launcher, DShK (C) |
60x130mm Rockets, 1120x12.7mm |
Type 89 MRL
Notes:
This is a large-capacity multiple rocket launcher on the same chassis as
the Type 83 gun/howitzer. The
turret is removed and replaced with the MRL and associated equipment and an
extra rocket pack and elevation and reloading equipment to reload the MRL.
(Reloading takes 3 minutes and does not require the crew to leave the
armor envelope of the hull.) The rocket pack is the same as mounted on the Type
81 MRL, and there is an additional rocket pack carried on the front deck.
The driver sits up front on the left, the commander is to the right of
the extra rocket pack between it and the active rocket pack, and is armed with a
machinegun, and the rest of the crew is in the rear under the rocket launcher.
The crew is protected by NBC Overpressure and has air conditioning.
Unlike most heavy MRLs, the Type 89 has full armor protection for the crew;
however, the rocket packs themselves are not so armored.
This vehicle has automatic laying and reloading systems that allow the
MRL to fire accurately without the assistance of an FDC is the target location
is known. The vehicle is powered by a 12V150L turbocharged diesel with an output
of 520 horsepower. Most other technical details are the same as the rocket
launcher of the Type 81.
This vehicle is
in service only with China.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$305,596 |
D, A |
500 kg |
30 tons |
5 |
17 |
Passive IR (D) |
Shielded |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
141/71 |
39/20 |
885 |
193 |
Trtd |
T4 |
TF2 TS2
TR2 HF16
HS6 HR6* |
Fire Control |
Stabilization |
Armament |
Ammunition |
+1 |
None |
40-round 122mm Rocket Launcher |
80x122mm Rockets, 1000x12.7mm |
*The armor value listed is for the vehicle chassis only.
The active rocket pack has an AV of 2; the stored spare rocket pack has
an AV of 4.
Type 762 MRL
Notes:
This MRL is similar to the Type 89 MRL in that they use the same chassis,
that of the Type 83 SP howitzer. This Chinese multiple rocket launcher was
specifically designed to clear minefields by blast, but can also be used to
destroy large troop concentrations and structures.
It consists of a pair of short-ranged 425mm rockets with fuel-air
explosive warheads to create overpressure for predetonating minefields, on a
tracked, armored chassis. The
typical rocket can clear an area 12x22 meters in size of mines, regardless of
type and how many arein the area. The launcher may be depressed to +6 degrees,
and elevated to +45 degrees.
Traverse is limited to left or right 10 degrees, and is primarily used to
fine-tune firing coordinates. The Type 762 inherits the rear door from Type 83
SPH. Also inherited from the Type 83 is its suspension and its 520-horsepower
engine. As it is a vehicle for a very specialized role, fire control equipment
is limited, as it would normally be only in narrowly-confined
circumstances. There is a machinegun mount by the commander's hatch and one
firing port on each side of the crew compartment.
The interior is NBC-sealed.
It should be
noted that while the Type 762 has decent cross-country mobility, it is also
vulnerable to side slopes, since the rockets may be depressed only so far and
this makes the Type 762 a bit top-heavy.
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
$1,535,139 |
D, A |
364 kg |
27 tons |
4 |
14 |
Passive IR (D) |
Shielded |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
153/78 |
42/22 |
885 |
193 |
Trtd |
T4 |
TF2 TS2
TR2 HF16
HS6 HR6 |
Fire Control |
Stabilization |
Armament |
Ammunition |
None |
None |
Twin 425mm Rocket Launchers, PKT (C) |
2x425mm Rockets, 500x7.62mm |
WM-80
Notes: A
greatly-updated Type 82 273mm MRL, the chassis used by the WM-80 is the 8x8
Taian TA5380 heavy truck, equipped with automatic transmission and a
turbocharged diesel engine developing 517 horsepower. All wheels have shock
absorbers and the tires are run-flat and puncture resistant. The cab is enlarged
to fit the entire crew, including reloaders, and fire control and navigation
equipment. This cab also has a
modicum or armor protection, and has NBC Overpressure and a filtered AC system.
The loaders are only there to ensure a positive lock between the old
launcher boxes and new pods then reloading. The second place in front and the
assistant gunner’s position is taken up by navigation and fire control
equipment; the rear seat has the commander and the two loaders that are part of
the crew. The commander has a hatch
above him, but there is no weapon mount around it.
The rockets may be fired singly or ripple-fired.
The launcher is mounted on an electrically-actuated turntable; elevation
range is +20 to +60, while traverse (facing front is left or right 20 degrees.
Four stabilizing jacks, one at each corner, are lowered before firing,
Battery control is normally done by an FDC, though in a pinch the WM-80
can provide rough coordinates and act as its own FDC.
To facilitate this, the WM-80 has GPS
with an inertial backup, self-surveying capability, and the ability to provide
its own coordinates if the target is known and on the maps on the mapping module
system. Note that which such
self-generated fire, medium and long-range fire has double scatter.
The WM-80 has
optronic and night vision devices in the launcher.
Reloading a launcher takes 5-8 minutes, depending upon the quality of the
crew. These loaders are not part of
the WM-80 crew, and ride in the ammo resupply trucks. It should be noted that a
larger variety of warheads are available to the 273mm rockets on the WM-80, and
they tend not to be used for minefield breaching anymore, though the FAE warhead
is retained.
The WM-120 is
essentially the same vehicle as the WM-80, but the rockets use more advanced
propellant, allowing 50% greater range.
This version is used by China and Peru, and is replacing the WM-80s used
by Jordan. Replacing the WM-80 with
the WM-120 is easy, as it merely requires an upgrade of the fire control
equipment and replacement of the rockets.
The WM-120 rockets also come in guided versions (similar in concept to
the US GMLRS), guided by inertial navigation with GPS terminal guidance, and
this type of use is included in the new fire control equipment.
By the time that
the WM-80 was ready for service, it was considered obsolete by the PLA, though
they are used by Armenia and Jordan. Turkey is considering a purchase, but they
have a list of upgrades they want done first. The WM-80 was in Chinese service
for only a very short time, replaced with the A-100 MRL, and to an extent by the
WM-120.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological* |
WM-80 |
$430,029 |
D, A |
693 kg |
34.7 tons |
6 |
26 |
Image Intensification, FLIR (D) |
Shielded |
WM-120 |
$470,079 |
D, A |
686 kg |
34.8 tons |
6 |
26 |
Image Intensification, FLIR (D) |
Shielded |
Vehicle |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
WM-80 |
125/63 |
34/18 |
770 |
191 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
WM-120 |
125/63 |
34/18 |
770 |
192 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
WM-80 |
+2 |
None |
4-Round 273mm Rocket Launcher |
4x273mm Rockets |
WM-120 |
+3 |
None |
4-Round 273mm Rocket Launcher |
4x273mm LR Rockets |
CPMIEC WS-1
Notes: In the
late 1990s, the PLA commissioned a new MLRS system, essentially to compete with
the US M270 MLRS on the international market and for domestic use. Also known as
the M-1, the WS-1 was also meant to bridge the gap between conventional
artillery and artillery rocket systems.
The WS-1 would generally have been considered a success for most such
projects: it fired huge rockets with large warheads and while range was not
stunning, it could still reach 80 kilometers.
However, the PLA was not impressed; the rockets had a minimum range of 20
kilometers (meaning they could not be fired at a target closer than 20
kilometers, the PLA was expecting significantly more range from the rockets, and
the launcher could mount only four rockets. They
called an end to the project after only a couple of prototypes were produced,
and not even LRIP was undertaken.
The statistics given below are highly conjectural, as detailed statistics for
the WS-1 have never been released.
The Khaibar-1
The Khaibar-1
(also known as Khyber-1, M-302, and B-302) was an almost complete clone of the
WS-1. The customer was ostensibly
Syria; however, the Syrians had no real interest in acquiring the WS-1 – it was
essentially a straw purchase for Hezbollah and Hamas, giving them longer-ranged
and more powerful rockets with larger warheads to pummel Israel.
The fire control system is somewhat dumbed down, and the base chassis is
a Russian-made heavy truck with about the same capabilities as the WS-1, The TEL
is also Syrian-designed and meant to require minimal maintenance.
For game purposes, the Khaibar-1 is identical to the WS-1.
The WS-1B
The WS-1B was
developed from the ashes of the WS-1 program and is a Chinese large-caliber
multiple rocket launcher on a Taian TA5380 8x8 heavy truck chassis.
Known users include the PLA, Turkey (who builds the WS-1B and its rockets
under license).and Thailand (who get knock-down versions from China but they are
assembled in Thailand). The launch system of the WS-1B may handle launchers of
four or eight rounds. These are
large rockets (they have longer propellant section than those of the WS-1).
which may use any of several warheads.
The WS-1B may also mount and fire the larger WS-1 rockets. Though the cab
is extended, only three operators are required; behind the cab is a large module
containing the computers, radios, and electronics for the vehicle.
The base chassis has a flatbed, on which is mounted a turntable to
traverse and elevate the rocket launcher.
Included in the electronics are a digital computer that increases
accuracy of the rockets. The MRL and association erection equipment completely
fills the cargo area, except for a small area behind the cab.
The WS-1B includes a vehicle state computer.
T-300 Kasiga
The T-300 (also
known as the TRG-300) is the Turkish version of the WS-1B.
It uses a German MAN 26.372 6x6 chassis as a base; this is not quite as
large as the Taian TA5380, but the chassis is heavier than the Taian TA5380 and
it uses a 550-horsepower engine with locking differentials and antilock brakes,
along with an automatic transmission, antilock and power brakes, and power
steering. The cab windows have armored shutters; these are primarily for crew
protection from the blast of the rockets than for general protection.
The missiles are the same as those of the WS-1B, and the fire control is
a Turkish-designed system, as is the observation system, and most of the Turkish
electronics suite duplicates the original Chinese equipment.
However, the T-300 also has a BMS.
The WS-2
This MRL was
revealed in 2004 at the Zhuhai Air Show.
It uses purpose-built 400mm rockets, with warheads ranging from
conventional to the exotic, from HE and DPICM to a version which launches three
UAVs which home in on radar emissions. (Rumors state that the Chinese bought the
specifications for the Israeli Harpy UAV to develop their submunition UAVs.)
Officially, the range of the rockets is 200 kilometers, but some sources
say it’s more like 350 kilometers.
The chassis is the same as that of the WS-1B, but the launcher has box-like
launchers for four rockets.
The WS-2B uses
the same firing equipment and truck, but the rockets use different propellant
and is able to carry a heavier warhead to the same range.
The WS-2C is a
GMLRS system with GPS-guided missiles, and having a range of 350 kilometers.
If the GPS signal is lost, the missile may guide itself (at a penalty of
-2 to hit) using passive homing guidance.
There is no UAV-launching round for the WS-2C.
The WS-2D is
also a GMLRS, but carries a smaller warhead out to 400 kilometers, and does have
two UAV-launching rounds – the ARM UAVs as above, and SADARM-type UAVs.
The WS-3
Though built on
the same truck chassis, the electronics of the launch system are updated, as the
WS-3 fires different missiles. The
WS-3 series are GLMRS launchers, and progressive versions of the WS-3 have a bit
more tech in their guidance units than previous models in the series, and better
propulsion units. The base WS-3 has
six launch boxes each with one 406mm missile.
The missiles are launched in the direction of the target, and then
midcourse inertial guidance takes over and guides the missiles to the target.
The WS-3A uses a
combination of inertial guidance with midcourse and terminal update guidance
provided by GPS or GLONASS (depending on the buyer).
The WS-3 series
is designed specifically for export and not used by the PLA.
Twilight 2000
Notes: This vehicle was just beginning to be produced before the Twilight War
and was in short supply.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological* |
WS-1 |
$571,077 |
D, A |
645 kg |
17.2 tons |
3 |
9 |
Thermal Imaging, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-1B |
$642,815 |
D, A |
500 kg |
17.2 tons |
3 |
9 |
Thermal Imaging, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
T-300 Kasiga |
$673,158 |
D, A |
555 kg |
20.1 tons |
3 |
17 |
FLIR, 2nd Gen Image Intensification (G, C, D), 3xCCD Cameras
(G, C) |
Shielded |
WS-2 |
$1,779,870 |
D, A |
606 kg |
19.35 tons |
3 |
12 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-2B |
$1,815,417 |
D, A |
620 kg |
19.66 tons |
3 |
12 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-2C |
$1,848,750 |
D, A |
622 kg |
19.66 tons |
3 |
14 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-2D |
$1,878,750 |
D, A |
624 kg |
19.66 tons |
3 |
14 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-3 |
$2,593,174 |
D, A |
498 kg |
19.81 tons |
3 |
14 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
WS-3A |
$2,596,841 |
D, A |
422 kg |
19.81 tons |
3 |
14 |
FLIR, Image Intensification (G, D), 2xCCD Cameras |
Shielded |
Vehicle |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
WS-1/1B |
220/110 |
61/30 |
775 |
193 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
T-300 Kasiga |
203/102 |
57/29 |
400 |
203 |
Stnd |
W(3) |
TF2 TS2
TR2 HF2
HS2 HR2 |
WS-2 |
195/100 |
54/27 |
775 |
186 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
WS-2B/2C/2D |
193/98 |
53/28 |
775 |
188 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
WS-3/3A |
195/98 |
56/27 |
775 |
193 |
Stnd |
W(5) |
TF2 TS2
TR2 HF2
HS2 HR2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
WS-1 |
+2 |
None |
4-Round 320mm Rocket Launcher |
4x320mm Rockets |
WS-1B/T-300 |
+2 |
None |
4-Round 302mm Rocket Launcher |
4x302mm Rockets |
WS-2 |
+3 |
None |
6-Round 400mm Rocket Launcher |
6x400mm Rockets |
WS-2B |
+3 |
None |
6-Round 400mm Rocket Launcher |
6x400mm LR Rockets |
WS-2C/2D |
+3 |
None |
6-Round 400mm Missile Launcher |
6x400mm Missiles |
WS-3/3A |
+3 |
None |
6-Round 406mm Missile Launcher |
6x406mm Missiles |