Lockheed Martin/BAE M142 HIMARS
Notes:
HIMARS (High-Mobility Artillery Rocket System) is a light rocket launcher
mounted on an M-1083 MTV 5-ton truck chassis.
The rocket launcher uses one module of the same rockets as the MLRS, on a
lightweight launcher assembly. The
HIMARS, however, mounts only one pod of launchers instead of the two of the
MLRS. The system was designed to be transported aboard C-130 aircraft, or sling
loaded below heavy-lift helicopters.
In addition to US Army use (mostly in light, airborne, and air assault
divisions), the US Marines have also adopted the HIMARS.
Singapore, UAR, Poland, and Romania use the HIMARS, and Canada, Qatar,
and the Philippines are considering its use.
The British are also considering use of the HIMARS, though theirs are
being tested using the chassis of the Supacat 600 truck. The US Army began
fielding them in 1998, while the Marines began fielding them in 2007.
The Taliban in Afghanistan are known to have captured at least one HIMARS
launcher and an unknown quantity of 227mm rockets, and have used them in one
attack on US and British units in Kandahar in 2010.
The US has deployed a number of HIMARS launchers to provide fire support
to US forces in Northern Syria and Iran.
The HIMARS are also known to be supporting PKK forces as well as the
forces of Syrian Democratic Forces.
The fire control
computers, command and control system, and launcher module are all the same as
on the MLRS, but the entire system is much lighter, with many of the components
being of newer technology and miniaturized.
Being an FMTV
variant, the HIMARS uses a Caterpillar C7 330-horsepower engine turbocharged
diesel engine with an automatic transmission. It also has power steering, with
additional boosting on the front wheels. Suspension uses leaf springs, assisted
by pneumatic shock absorbers and an anti-roll bar on the rear wheels. The cab
and rocket pod have a modicum of armor, as well as metal shutters to close over
the windshields when firing, to avoid damaging the windows. The cab has NBC
Overpressure protection and an air conditioner with NBC filters, as well as a
BMS including GPS navigation, self-surveying capability, and no need for an FDC.
The crew does not need to leave the vehicle to launch its rockets, and with
special reloading vehicles, the HIMARS crew and the reload crew do not need to
leave their vehicles to reload the HIMARS.
The HIMARS has
also been tested on ships, mounting the launchers directly on the amphibious
transport dock ship USS Anchorage. Tests have also been conducted with
the entire HIMARS truck firing from the flight deck of amphibious assault ships.
The HIMARS’s fire control software was modified to allow accurate fire from a
rolling and moving ship. The HIMARS has also been tested as a SLAMRAAM platform
(Surface-Launched AMRAAM), with the addition of a radar set and modification of
the fire control system. The
SLAMRAAM HIMARS can also fire regular 227mm rocket pods. The HIMARS system may
also fire a single ATACMS missile from a special pod instead of a normal MLRS
pod.
Twilight 2000
Notes: This weapon system was deployed to the 82nd and 101st
Airborne Divisions in early 1997, as well as to some light infantry divisions
and separate brigades; the Army gave the Marines 20 of these launchers and an
ample number of rockets. Note that
the Marines did not have the ATACMS missile, though they did have the SLAMRAAM
system. Later in the war, with
AIM-120 missiles in short supply, the SLAMRAAM system was modified to use
SL-Sparrow missiles and SL-Sea Sparrow missiles.
Merc 2000 Notes:
By 2012, deployment of the HIMARS began to exceed that of the MLRS.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
HIMARS w/MLRS Rockets |
$525,068 |
D, A |
552 kg |
16.2 tons |
3 |
18 |
Headlights |
Shielded |
HIMARS w/ATACMS Missile |
$749,716 |
D, A |
624 kg |
16.04 tons |
3 |
18 |
Headlights |
Shielded |
HIMARS w/SLAMRAAM Missiles |
$749,716 |
D, A |
395 kg |
15 tons |
3 |
19 |
Radar (75 km) |
Shielded |
Vehicle |
Tr Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config |
Susp |
Armor |
HIMARS w/MLRS Rockets |
144/101 |
40/28 |
212 |
122 |
Trtd |
W(3) |
TF2 TS2
TR2 HF2
HS2 HS2 |
HIMARS w/ATACMS Missile |
145/102 |
40/28 |
212 |
122 |
Trtd |
W(3) |
TF2 TS2
TR2 HF2
HS2 HS2 |
HIMARS w/SLAMRAAM Missiles |
153/107 |
43/30 |
212 |
122 |
Trtd |
W(3) |
TF2 TS2
TR2 HF2
HS2 HS2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
HIMARS w/MLRS Rockets |
+2 |
None |
6-Round 227mm Rocket Launcher |
6x227mm Rockets |
HIMARS w/ATACMS Missile |
+3 |
None |
1-round ATACMS Missile Launcher |
1xATACMS Missile |
HIMARS w/SLAMRAAM Missiles |
+2 |
None |
6-Round AMRAAM Missile Launcher |
6xAMRAAM Missiles |
Vought/Boeing M270 MLRS
(Multiple Launch Rocket System)
Notes:
When this vehicle entered US Army service in 1983 after a lengthy
development period; the initial request for such a vehicle was issued in 1974.;
The M270 was the first multiple rocket launcher used by the US military since
the late 1950s. 12 other countries
around the world, mainly in NATO armies, also used it, with Israel being the
first export order. In combat, the main users of the MLRS have been Israel, the
US, The basic HE rocket was used with great success in the 1991 Persian Gulf
War, along with DPICM,.but since then, a plethora of new and improved rockets
have been devised, including the guided 227mm rockets recently devised.
One arms expert stated that a full ripple from an MLRS has the
effectiveness of 33 155mm cannon artillery guns, and at a much longer range.
The M270
(generally referred to by the troops as the “MLRS”)
is mounted on a lengthened Bradley chassis, and carries two pods with six
227mm rockets each. The barrage of
rockets was known in the US Army as a “Grid Square Weapon,” able to bombard an
entire 1000x1000 meter 4-digit grid square found on NATO military maps with one
ripple of rockets. The MLRS is
normally resupplied from modified MLRS chassis which uses a crane and
stabilizing equipment to reload the MLRS without the crew of the launcher or the
resupply vehicle having to leave their vehicles Sometimes, logistics carriers or
special trailers towed by HEMTT trucks carry the reloads, and the reload crew
must leave their vehicles to do the reloading..
The M270 is
capable of operating without the assistance of an FDC, needing only coordinates
from a FIST team, and able to fire accurately within 30 seconds (6 phases) of a
halt. Its integrated GPS and
mapping computer enables this. This
capability also allows the individual MLRSs in a battery may spread out over
long distances and still bombard the same target.
Being based on
an M2 Bradley chassis, the M270 has a multifuel turbocharged engine developing
600 horsepower, with power automatic transmission and power brakes.
The engine can run off of diesel (used by most countries using the MLRS),
or JP8 jet fuel (used primarily by the US).
An alcohol/diesel combination of up to 20% ethanol may be used without
modification or hurting performance, but the use of pure alcohol requires
considerable changing of engine parts.
The M270 and its specialist loader vehicle have 12kW APUs to allow the
system to function to operate with the engines off; this APU runs off vehicular
fuel and is protected by the MLRSs (modicum of) armor.
The cab houses the entire crew, and has shutters which can be closed over
the windshields and windows to protect them during rocket launch.
The pods themselves are disposable, though the empty pods may be returned
to rear areas for refurbishment and reloading.
The ATACMS (Army
TACtical Missile System) is a large, guided missile that has more range and
precision than the MLRS. This was
introduced with the M270 IPDS upgrade, and was not applied to all MLRSs. The
ATACMS can be fired from any properly-equipped MLRS vehicle, from a two-missile
box. The ATACMS is fired using
Average: Heavy Artillery at a +4 modifier, or may be fired using Easy: Guided
Weapon skill. The ATACMS is used
only by the US, Greece, South Korea, and Turkey.
Other
modifications and versions include the M270A1, which has an upgraded fire
control system and an improved launcher able to elevate and depress a little
more. In addition to allowing for longer and shorter-range shots, the reloading
time was somewhat shortened. The
M270A1 modifications allowed for the firing of newer ammunition types. The
M270A1 can also fire the then-new (in 2005) GMLRS GPS-guided missiles.
The M270B1 is
used by Britain; it has a bit more armor, especially in the cab and vehicle
floor. It also upgrades their MLRSs to the M270A1 standard.
The M270
MARS2/LRU uses a European designed (largely by Airbus) enhanced fire control
system. It is capable of firing the
full range of MLRS rockets and missiles (except ATACMS).
It can also mount pods containing 110mm LARS rockets. Note that while the
MARS2/LRV is capable of using DPICM, warheads, the Germans, Italians, and French
have elected to abide by the new Convention on Cluster Munitions and do not
employ DPICM warheads, though they have devised an enhanced HE/FRAG warhead. It
otherwise has the M270B1 improvements.
The M270D1
further improves the FCS and its ability to fire and guide GMLRS and ATACMS
missiles, as well as fire the full range of MLRS rockets.
Current operators include the US, Britain, Bahrain, and Finland.
These later M270s are
also equipped with a BMS and vehicle state system.
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
M270 |
$418,998 |
D, A |
671 kg |
24.95 tons |
3 |
21 |
Headlights |
Shielded |
M270 IPDS |
$510,031 |
D, A |
681 kg |
24.7 tons |
3 |
22 |
Headlights |
Shielded |
M270A1 |
$622,698 |
D, A |
703 kg |
24.5 tons |
3 |
23 |
Headlights |
Shielded |
M270B1 |
$675,528 |
D, A |
708 kg |
24.9 tons |
3 |
23 |
Headlights |
Shielded |
M270 MARS2/LRU |
$727,528 |
D, A |
718 kg |
25.1 tons |
3 |
24 |
Headlights |
Shielded |
M270D1 |
$966,589 |
D, A |
733 kg |
24.7 tons |
3 |
23 |
Headlights |
Shielded |
Vehicle |
Tr
Mov |
Com Mov |
Fuel Cap |
Fuel Cons |
Config* |
Susp |
Armor |
M270 |
165/116 |
46/32 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF2 HS2
HR2 |
M270 IPDS |
166/116 |
46/32 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF2 HS2
HR2 |
M270A1 |
168/117 |
47/33 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF2 HS2
HR2 |
M270B1 |
165/116 |
46/32 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF3 HS3
HR3** |
M270 MARS2/LRU |
164/115 |
46/32 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF3 HS3
HR3** |
M270D1 |
166/116 |
46/32 |
617 |
222 |
Trtd |
T3 |
TF2
TS2 TR2
HF2 HS2
HR2 |
Vehicle |
Fire Control |
Stabilization |
Armament |
Ammunition |
M270 |
+2 |
None |
2x6-Round MLRS
Rocket Launchers (Early) |
12x227mm Rockets
(Early) |
M270 IPDS |
+2 |
None |
2x6-Round MLRS
Rocket Launchers (Early) or 2xATACMS Missile Launchers (Early) or Mix |
12x227mm Rockets
or 2xATACMS Missiles or Mix (Early) |
M270A1/M270B1 |
+3 |
None |
2x6-Round MLRS
Rocket Launchers or 2xATACMS Missile Launchers or 2x6 GMRLS Missiles or
Mix |
12x227mm Rockets
or 2xATACMS Missiles or 12xGMRLS Missiles or Mix |
M270 MARS2/LRU |
+4 |
None |
2x6-Round MLRS
Rocket Launchers or 2x6-Round GMLRS Rocket Launchers or 2x10x110mm
Rocket Launchers or Mix |
12x227mm Rockets
of 12xGMRLS Missiles of 20x110mm Rockets or Mix |
M270D1 |
+4 |
None |
2x6-Round MLRS
Rocket Launchers or 2xATACMS Missile Launchers or 2x6 GMRLS Missiles or
Mix |
12x227mm Rockets
or 2xATACMS Missiles or 12xGMRLS Missiles or Mix |
*The “turret” in this case refers to the launcher and the erector mechanism; no
crew members can come to harm as a result of hits on the launcher, and such
results are considered misses.
**The cab is essentially in an armored capsule of sorts, with an AV of 3 from
all angles.