Mission:
The mission of Patriot is to provide protection for
critical assets and maneuver forces belonging to
corps and echelons above corps (EAC) against
airborne threats from very low to very high
altitudes. The objective of Patriot operations at
all levels is to disrupt and destroy the enemy's
ability to mount effective air operations.
SYSTEM DESCRIPTION - BATTALION FIRE
DIRECTION CENTER
The major end items of the Patriot battalion
fire direction center (FDC) are the Information and
Coordination Central (ICC) (AN/MSQ-ll6), Electric
Power Unit (EPU II) (PU 789), Communications Relay
Group (CRG) (AN/MRC-137) and Antenna Mast Group
(AMG) (OE-349/MRC).
INFORMATION AND COORDINATION CENTRAL
The ICC is the C3 center of the Patriot
battalion during AD operations. The ICC consists of
a lightweight weather tight shelter mounted on a
5-ton cargo truck (figure 1). The shelter provides
shielding from radio frequency interference (RFI)
and electromagnetic pulse (EMP) radiation. It is
equipped with two externally mounted air
conditioners that cool, heat, and ventilate the
interior. An externally mounted gas particulate
filter unit (GPFU) is used in NBC situations to
provide clean air for crewmembers.
The ICC contains two consoles that are manned
by the tactical director (TD) and tactical director
assistant (TDA). Between the two consoles is an ICC
status panel that displays the status of all
battalion fire units (FU).
Figure 1
ELECTRIC POWER UNIT
The EPU II is the prime power source for the
ICC and CRG. The EPU II consists of a 30 kw, 400 Hz
generator mounted on a trailer and towed by the ICC
or CRG. Two generators will be used for the ICC and
two generators for the CRG.
COMMUNICATIONS RELAY GROUP
The CRG provides a multirouted secure, two-way
data relay capability between the ICC, its assigned
fire units, and between adjacent units. The CRG also
provides the capability for both data and voice exit
and entry communication points with elements that
are external to Patriot.
ANTENNA MAST GROUP, TRUCK MOUNTED,
OE-349/MRC
The AMG (figure 2) is a mobile antenna mast
system used to carry the amplifiers and antennas
associated with the UHF communications equipment
located in the ECS, ICC, and CRG. Four antennas are
mounted in two pairs, are remotely controlled in
azimuth, and can be elevated to heights up to 100
feet, 11 inches, above ground level.
Figure 2
SYSTEM DESCRIPTION - FIRING BATTERY
The heart of the Patriot battery is the fire
control section and associated launchers. The major
end items are the Engagement Control Station (ECS)
(AN/MSQ-104), Electric Power Plant (EPP III)
(M977EPP), Radar Station (RS) (AN/MPQ-53), eight
Launching Stations (LS) (M901) and Antenna Mast
Group (AMG) (OE-349/MRC). A general description of
end items including the purpose and characteristics
follows.
ENGAGEMENT CONTROL STATION TRUCK MOUNTED
AN/MSQ-104
The ECS is the operational control center of
the Patriot FU (figure 3). It contains the WCC,
man/machine interface and various data and
communications terminals. The ECS is air-conditioned
and includes protection devices for use in NBC and
EMP environments.
The ECS shelter provides shielding from RFI
and is a weather-tight enclosure with appropriate
air inlet and exhaust ports for the environmental
control systems. The left side as seen from the
doorway includes three UHF RRT and a voice
communications station. The right side includes the
very high frequency (VHF) DLT, radar weapon control
interface unit (RWCIU), WCC, an AN/VRC-92A SINCGARS
radio, optical disc drives (ODD) and embedded data
recorder.
Figure 3
RADAR SET, SEMI-TRAILER MOUNTED, AN/MPQ-53
The RS consists of a multifunction phased
array radar mounted on an M-860 semi-trailer towed
by an M983, heavy expanded mobility tactical truck
(HEMTT) (figure 4). It is monitored and controlled
by the ECS via the radar and weapon control
interface unit. It performs very low- to very
high-altitude surveillance, target detection, target
classification, target identification, target
track, missile track, missile guidance, and ECCM
functions.
The radar antenna is positioned at the forward
end of the shelter and is erected to a fixed 67.5
angle relative to the horizontal plane during
emplacement. Integral leveling equipment on the
M-860 semi-trailer permits emplacement on slopes of
up to 10.
Figure 4
ELECTRIC POWER PLANT
The Electric Power Plant (EPP III) (figure 5)
is the prime power source for the ECS and RS. Each
EPP consists of two 150 kw, 400 Hz diesel engines
that are interconnected through the power
distribution unit (PDU) and are mounted on a 10-ton
M977 HEMTT. Each EPP contains two interconnected
75-gallon fuel tanks and a fuel distribution
assembly with grounding equipment. Each diesel
engine can operate more than eight hours with a full
fuel tank.
Figure 5
ANTENNA MAST GROUP, TRUCK MOUNTED,
OE-349/MRC
The AMG (figure 2) is a mobile antenna mast
system used to carry the amplifiers and antennas
associated with the UHF communications equipment
located in the ECS, ICC, and CRG. Four antennas are
mounted in two pairs, are remotely controlled in
azimuth, and can be elevated to heights up to 100
feet, 11 inches, above ground level.
Emplacement consists of stabilizing the AMG,
setting the antenna feed and the erection of the
antennas by the use of self-contained hydraulic and
pneumatic systems and then adjusting the antenna
elevation. Connecting cables to the collocated
shelter is carried on the AMG and includes RF
cables, control cables, and a prime power cable.
LAUNCHING STATION, GUIDED MISSILE SEMI-TRAILER
MOUNTED
The Launching Station (LS) (figure 6) is a
remotely operated, fully self-contained unit, that
has integral onboard power and carries up to four
guided missiles (PAC-2), or 16 missiles (PAC-3).
Operation is controlled in the ECS via fiber optics
or VHF data link. The LS is mounted on an M-860
semi-trailer towed by an M983 HEMTT. Leveling
equipment permits LS emplacement on slopes of up to
10. The LS is trainable in azimuth 110 and elevates
to a fixed, elevated, launch position. The LS has to
be precisely emplaced and aligned prior to launch.
Proper emplacement and alignment is critical for
engagement of ballistic missiles.
The Launching Station contains four major
equipment subsystems. The four subsystems are as
follows:
- Launcher
generator set: the onboard source of LS
electrical power.
- Launcher
Electronics Assembly: two trailer-mounted
equipment consoles that receive, decode, and
execute commands of the ECS.
- Launcher
Mechanics Assembly: elevates the guided missiles
and contains a data link antenna mast for
communications with the ECS.
- Launcher
Interconnection Group: interconnects onboard LS
equipment and controls the routing of electrical
function lines to and from the guided missiles.
GUIDED MISSILE
INTERCEPT AERIAL, MIM-104
The missile, from
front to rear, consists of a radome, guidance
section, warhead section, propulsion section, and
control actuator section. The Patriot missile is
mounted within a canister (figure 7) that
functions as a shipping and storage container and
as a launch tube. Guided missile canisters are
stacked into groups of four per LS (PAC-2).
Figure 7
A desiccant
indicator on the aft end of the canister monitors
the humidity. A single umbilical cable connection
interfaces the canister with the LS and provides
the means for status monitoring, preheating, and
launching.
The missile has
four clipped-delta, movable, tail-control
surfaces, and is propelled by a single-stage,
all-boost solid-propellant rocket motor (figure
8). BITE checks missile readiness and provides GO
or NO-GO logic for successive events in the
countdown. A malfunction in any lead-in event in
the missile activation and arming sequence will
prevent rocket motor ignition. Any defect is
automatically reported to the WCC in the ECS.

Figure 8
The standard
Patriot missile (MIM-104) was the first type
fielded and contained an analog fuze. This fuze
was replaced by a digital version with the
fielding of the MIM-104A. Both of these missiles
provide excellent performance against ABTs and
adequate performance against TBMs.
To counter the
long-range ECM threat the MIM-104B, or standoff
jammer countermeasures (SOJC) missile, was fielded
in the late 1980s. The guidance and
navigation hardware was modified to allow the SOJC
missile to fly a lofted trajectory to the jamming
source and seek out the strongest emitter during
the terminal phase of missile flight. The SOJC
missile can fly three times longer than the
standard missile without the uplink/downlink
between the RS and missile. The SOJC missile
retains the same performance against ABT and TBM
as the standard missile.
The Patriot
Advanced Capabilities 2 (PAC-2) missile, MIM-104C,
was fielded during Operation Desert Shield and
Operation Desert Storm to counter the advanced TBM
threat. A new warhead and dual-mode fuze was added
to the missile. The new warhead contains a more
powerful explosive and larger fragments designed
to place sufficient kinetic energy on the warhead
section of threat TBMs to achieve a Warhead Kill.
The dual-mode fuze allows the PAC-2 missile to
retain ABT performance and also optimize
performance against TBM. The system software based
on the mission selected for the missile sets the
fuze mode.
The Guidance
Enhancement Missile (GEM) is an improved PAC-2
missile. A Low Noise Front End (LNFE) and improved
fuze have increased lethality and expanded TBM
engagement volume.
The Patriot
Advanced Capability (PAC-3) missile is to be
incorporated into the Patriot air defense system.
It will provide defense against tactical ballistic
missiles, advanced cruise missiles, and other
air-breathing threats in the presence of
electronic countermeasures and rough terrain.
Rather than
relying on proximity detonation that can simply
redirect or break up an incoming threat, the PAC-3
missile hits the target warhead to assure complete
destruction. The PAC-3 missile achieves its
hit-to-kill capability through the combination of
an extremely accurate seeker coupled with
exceptionally rapid airframe response. The missile
also utilizes a lethality enhancer that is
designed to increase the performance against
air-breathing threats. There are 16 PAC-3 missiles
per Patriot launcher (versus four PAC-2 missiles
per launcher) and eight launchers per Patriot
battery. |