01-02-2004, 00:32
PALADIN 155MM - SPECIFICATION
Armament and ammunition
Cannon range unassisted 24 km
Cannon range assisted 30 km
Projectile loading Semi-automatic
Ammunition capacity 39 complete rounds
Rate of firing
Response time <60 seconds
Sustained rate of fire 1 round/3 minutes
Maximum rate of fire 3 rounds/15 seconds; 8 rounds/minute
Fire control Automatic fire control with optical backup
Navigation Inertial positioning navigation system integral with AFCS
Mean time between failure 122 hours
Mean time to repair 2 hours
Optics night vision compatible
NBC protection individual crew protection with heating and cooling
Hydraulic segregated hydraulics system
Combat weight 63,600 lbs
Length 384 inches
Width 124 inches
Height 127.4 inches
Ground clearance 18 inches
Ground pressure 113.53 psi
Fuel capacity 133 gallons
Speed 40 mph
Vehicle range 214 miles
Engine DDEC 8V71T, 2 cycle diesel, 440 horsepower
Transmission 4 forward, 2 reverse
Suspension torsion bar high strength with high capacity shock absorbers
Electrical power 650 amps, 24 v DC
Travel clock remote powered
Communications VIC-1, VRC-89 or SINCGARS
Cost is $8.0Million
CRUSADER 155MM - SPECIFICATION
Lethality
Rate of fire 10 rounds per minute
Gunpointing Fully automated
Ammunition handling Fully automated
Ready to fire 15 to 30 seconds
Time on target 4 rounds from 5-30 km
Minimum range 5 km
Maximum range 40+ km
Mobility
Road speed 67 km/hr
Cross-country speed 48 km/hr
Deployability
Footprint Same as Paladin/ FAASV
Air transport C-5 and C-17 transportable
Predicted munitions effectiveness 2X Paladin
Survivability
Displace/move profile 750 meters/ 90 seconds
Active defence system Integrated, remote controlled, active defence system
Sustainability
Maintenance aids Embedded diagnostics/prognostics
Ammunition upload/transfer Fully automated
Crew size 3
Resupply 60 rounds of ammunition and fuel in 12 minutes
Power pack
Engine Crusader CV12 1500 engine provided by Perkins and Caterpillar
Transmission HMPT 15O0-EC Transmission from General Dynamics
Power Takeoff Full power, constant running
Service and Parking Brakes Mechanically actuated, oil-cooled, multiple disc power
Dynamic Steering Full engine retarding torque/limited hydrostatic
Steering True pivot steering, continuously variable ratio hydromechanical, fully regenerative without brakes/clutches
Input disconnect Hydraulically actuated clutch power train disconnect
Suspension External hydropneumatic
Track Improved M1A2/Tl 5BLL track
Control systems Drive-by wire/Position navigation/Movement planning decision aids
Cost is $8.2Million
PZH 2000 155MM - SPECIFICATION
Crew 5 (commander, driver, gunner, two ammunition loaders)
155 millimetre Gun
Calibre 52
Range with NATO ammunition 30 km
Range with base bleed ammunition 36.5 km
Range with assisted projectiles 40 km
Demonstrated performance Multiple round simultaneous impact capability (MRSI) and firing on moving targets
Resupply 60 rounds and 288 charges by 2 crew members, less than 10 min 50 sec
More than 26,300 km of road and cross country driving
Execution of nine 24 hour battlefield days, with, 9 x 300 rounds from 37 different firing positions, and 9 x 125 km moves
Firing rate demonstrated using 24 volt technology automatic loader
Firing rate 3 rounds in 9.2 seconds
Firing rate 8 rounds in 42.9 seconds
Firing rate 10 rounds in 59.6 seconds
Sustained firing rate 20 rounds in 2 minutes 10 seconds
Firing rate demonstrated using 48 volt technology automatic loader
Firing rate 3 rounds in 8.4 seconds
Firing rate 12 rounds in 59.74 seconds
Sustained firing rate 20 rounds in 1 minute 47 seconds
Dimensions
Hull length 7.9 metres
Overall length 11.7 metres
Barrel overhang 3.3 metres
Width 3.6 metres
Height 3.1 metres
Combat weight 55 tons
Power
Powerpack MTU type 881
Power to weight ratio 13.4 kW/ton
Rating 736 kW
Transmission Renk HSWL 284C
Vehicle performance
Highway speed greater than 60 km/hour
Typical tank cross country speed greater than 45 km/hour
Radius of action 420 kilometres
Transportability STANAG 2832 B
Forward slope 50%
Trench crossing 3 metres
Cost is $5.0Million
MSTA-S 2S19 152MM - SPECIFICATION
152 mm howitzer
Armament
12.7 mm machine gun
Maximum firing range
HEF projectile 24.7 km
HEF gas-assisted projectile 28.5 km
Minimum firing range 6.5 km
Maximum rate of fire 8 rds/min
Elevation +68 to -3 degrees
Traverse 360 degrees
HEF projectile weight 43.56 kg
Onboard ammunition load
152 mm 50 rounds
Machine gun 300 cartridges
Mount weight 42.5 tons
Crew 5
Road speed 60 km/hr
Road range 500 km
Dimensions
Length (gun forwards) 11.91 m
Width 3.3 m
Height (to turret top) 2.98 m
Obstacles
Gradient 47%
Side slope 36%
Trench width 2.8 m
Power-to-weight ratio 18.5 - 20 hp/t
Vertical obstacle 0.5 m
2K25 KRASNOPOL PRECISION-GUIDED MUNITION
Calibre 152 mm
Warhead HE-FRAG
Guidance inertial and semi-active laser homing
First shot fixed target hit probability 0.9
Firing range
Maximum 22 km (from 2S19 MSTA-S)
Minimun 3 km
Range of tank type target (illuminated by 1D22) 7 km
Length 1300 mm
Weight
Projectile 50 kg
Warhead 20.5 kg
Explosive 6.4 kg
Cost is $6.0Million
TIGER - SPECIFICATION
Design mission weight 5400 kilograms
Alternate gross weight 6000 kilograms
Length 14 metres
Height 3.81 metres
Wing span 13 metres
Hover out of ground effect (OGE) 3200 metres, anti-tank version
3500 metres, combat support version
Vertical rate of climb 5.2 metres per sec, anti-tank version
6.4 metres per sec, combat support version
Maximum rate of climb 10.7 metres per sec, anti-tank version
11.5 metres per sec, combat support version
Flight speed, armed 145 knots, anti-tank version
155 knots, combat support version
Cruise speed 124 knots
Design limit speed 161 knots, anti-tank version
174 knots, combat support version
Maximum range, internal fuel 800 km
Mission endurance 2 hours 50 minutes
Maximum endurance, internal fuel 3 hours 25 minutes
Agility 40 degree angle of yaw after first second
Trigat missile range 500 metres to 5 kilometres
Maximum air to air missile range > 5 kilometres Maximum autonomous
Target identification and engagement 5 kilometres
Maximum internal fuel capacity 1020 kilograms
Maximum internal plus external fuel capacity 1575 kilograms
Cost is $15Million
AH-64A/D APACHE - SPECIFICATION
Crew 2 crew: pilot and copilot/gunner
Diameter main rotor blades 14,630 cm
Height 3,590 cm
Empty weight 5,352 kilograms
Maximum cruising speed 260 kilometres per hour
Maximum rate of climb 942 meters per minute
Maximum vertical rate of climb 474 meters per minute
Range 400 kilometres on internal fuel
1,900 kilometres on internal and external fuel
Maximum endurance 3 hours 9 minutes on internal fuel
The g limit values +3.5 g to -0.5 g
Cost is $15million.
AH-1W / AH-1Z SUPER COBRA - SPECIFICATION
Dimensions
Length 13.9 metres
Height 4.02 metres
Rotor diameter 14.63 metres
Powerplant 2 General Electric T700-401 rated at 1,625 shp
Weight
Empty weight 12,200 lbs (10,920 lbs)
Maximum gross weight 16,800 lbs (14,750 lbs)
Internal fuel 2755 lbs(2,086 lbs)
Maximum ordnance 3,914 lbs (1,661 lbs)
Hovering out of ground effect (HOGE) gross weight 16,600 lbs (10,300 lbs)
Performance
Maximum airspeed 210 knots (170 knots)
Cruise speed at altitude 3,000 ft and 91.5 deg F 148 knots (137 knots)
Cruise speed at altitude 4,000 ft and 95 deg F 137 knots (131 knots)
Maximum range with 20 minutes reserve fuel 350 nautical miles
Endurance with 20 minutes reserve fuel 3 hours 30 minutes (2 h 48 min)
Maximum g-load +3.2 g (+2.5g)
Minimum g-load -0.5 g (+0.5g)
Vertical rate of climb at altitude 3,000 ft 1,740 ft/minute (645 ft/minute)
Vertical rate of climb at altitude 4,000 ft 1,386 ft/minute (315 ft/minute)
Vertical rate of climb at altitude 5,000 ft 1,386 ft/minute (315 ft/minute)
Cost is $12Million.
S-70A BLACK HAWK - SPECIFICATION
Dimensions
Main rotor diameter 53 ft 8 inches
Tail rotor diameter 11 ft 0 inches
Overall length with rotors turning 64 ft 9 inches
Maximum height to top turning tail rotor 16ft 9 inches
Width fuselage 7 ft 9 inches
Weights
Empty weight 11,780 lbs
Mission gross weight 16,864 lbs
Maximum gross weight 22,000 Ibs
Engines
Two turboshaft engines General Electric T700-GE-701 C
Power 1,940 shaft horsepower
Transmission rating 3,400 shaft horsepower
Internal fuel 360 US gallons (1,360 litres)
External auxiliary fuel tanks on ESSS system 460 US gallons (1740 litres)
Endurance on internal fuel 3 hours 5 minutes
Maximum endurance with auxiliary fuel 7 hours 21 minutes
Performance
Performance figures at 16,864 lbs Missions Gross Weight:
Maximum Cruise Speed at 5,000 ft 162 kts
VNE (not to exceed speed) 190 kts
Service ceiling 19,000 ft
Hover ceiling, out of ground effect (OGE) 10,600 ft
Maximum range at 5,000 ft 304 nautical miles
Cost is $15Million.
CH-47D/MH-47E CHINOOK - SPECIFICATION
Dimensions
Overall length, rotors turning 30.2 m
Fuselage length 15.6 m
Distance between rotor centres 11.9 m
Width Fuselage 3.8 m
Overall height 5.8 m
Internal length 9.3 m
Internal width 2.3 m
Internal height 2.0 m
Accommodation 3 crew
Troop seats 44
Litters (stretchers) 24
Weight
Empty weight 10,578 kg
Maximum gross weight 24,494 kg
Useful load 13,916 kg
Forward and aft cargo hooks 9,072 kg
Centre cargo hook 12,701 kg
Performance
Sea level cruise speed 265 km/hour
Speed at maximum continuous power 269 km/hour
Rate of climb 464 metres per minute
Service ceiling 2575 m
Hover in ground effect 2,499 m
Hover out of ground effect 1,509 m
Range 426 km
Engines
Model two T55-L-712 SSB
Maximum shaft horsepower 2796 kW
Continuous shaft horse power 2237 kW
Rotor system 2 hubs, 3 blades per hub
Blades fibreglass
Speed 225 rpm
Diameter 18.29 m
Disc area 262.67 square m
Blade folding manual
Cost is $30Million.
T 80U - SPECIFICATION
Crew 3
Weight 46 tons
Engine GTD three shafts with two cascades of turbocompression power turbine and GTD-1250 controlled nozzle assembly
Power 1250 hp
Transmission mechanical, planetary
Track metallic with RMSh and rubber-tyred road wheels
Suspension torsion bar
Shock absorbers hydraulic, telescopic (on 1, 2 and 6 road wheels)
Electrical equipment 22 - 29 V DC
Starter storage batteries 4
Total capacity 340 A h
Radio receive/transmit, telephone, simplex, R-173
Intercom for four men R-174
Ground pressure 0.865 kg/sq cm
Road speed unpaved 40 - 45 km/hour
paved 60 - 65 km/hour
maximum 70 km/hour
Fuel consumption for 100 km
unpaved road 460 - 790 litres
paved road 430 - 500 litres
Fuel endurance
unpaved road 335 km (main fuel tanks)
400 km (with extra fuel drums)
paved road 500 km (main fuel tanks)
600 km (with extra fuel drums)
Negotiable obstacles
gradient 32 deg
side slope 30 deg
trench 2.85 m
Fording depth
without preparation 1.2 m
with preparation 1.8 m
with OVPT snorkel 5 m
Dimensions
length (gun forwards) 944.0Million
H Bombs
small compact
radiation will last for years
comes with a lauch carrirer
or can be used in a silo
Armament and ammunition
Cannon range unassisted 24 km
Cannon range assisted 30 km
Projectile loading Semi-automatic
Ammunition capacity 39 complete rounds
Rate of firing
Response time <60 seconds
Sustained rate of fire 1 round/3 minutes
Maximum rate of fire 3 rounds/15 seconds; 8 rounds/minute
Fire control Automatic fire control with optical backup
Navigation Inertial positioning navigation system integral with AFCS
Mean time between failure 122 hours
Mean time to repair 2 hours
Optics night vision compatible
NBC protection individual crew protection with heating and cooling
Hydraulic segregated hydraulics system
Combat weight 63,600 lbs
Length 384 inches
Width 124 inches
Height 127.4 inches
Ground clearance 18 inches
Ground pressure 113.53 psi
Fuel capacity 133 gallons
Speed 40 mph
Vehicle range 214 miles
Engine DDEC 8V71T, 2 cycle diesel, 440 horsepower
Transmission 4 forward, 2 reverse
Suspension torsion bar high strength with high capacity shock absorbers
Electrical power 650 amps, 24 v DC
Travel clock remote powered
Communications VIC-1, VRC-89 or SINCGARS
Cost is $8.0Million
CRUSADER 155MM - SPECIFICATION
Lethality
Rate of fire 10 rounds per minute
Gunpointing Fully automated
Ammunition handling Fully automated
Ready to fire 15 to 30 seconds
Time on target 4 rounds from 5-30 km
Minimum range 5 km
Maximum range 40+ km
Mobility
Road speed 67 km/hr
Cross-country speed 48 km/hr
Deployability
Footprint Same as Paladin/ FAASV
Air transport C-5 and C-17 transportable
Predicted munitions effectiveness 2X Paladin
Survivability
Displace/move profile 750 meters/ 90 seconds
Active defence system Integrated, remote controlled, active defence system
Sustainability
Maintenance aids Embedded diagnostics/prognostics
Ammunition upload/transfer Fully automated
Crew size 3
Resupply 60 rounds of ammunition and fuel in 12 minutes
Power pack
Engine Crusader CV12 1500 engine provided by Perkins and Caterpillar
Transmission HMPT 15O0-EC Transmission from General Dynamics
Power Takeoff Full power, constant running
Service and Parking Brakes Mechanically actuated, oil-cooled, multiple disc power
Dynamic Steering Full engine retarding torque/limited hydrostatic
Steering True pivot steering, continuously variable ratio hydromechanical, fully regenerative without brakes/clutches
Input disconnect Hydraulically actuated clutch power train disconnect
Suspension External hydropneumatic
Track Improved M1A2/Tl 5BLL track
Control systems Drive-by wire/Position navigation/Movement planning decision aids
Cost is $8.2Million
PZH 2000 155MM - SPECIFICATION
Crew 5 (commander, driver, gunner, two ammunition loaders)
155 millimetre Gun
Calibre 52
Range with NATO ammunition 30 km
Range with base bleed ammunition 36.5 km
Range with assisted projectiles 40 km
Demonstrated performance Multiple round simultaneous impact capability (MRSI) and firing on moving targets
Resupply 60 rounds and 288 charges by 2 crew members, less than 10 min 50 sec
More than 26,300 km of road and cross country driving
Execution of nine 24 hour battlefield days, with, 9 x 300 rounds from 37 different firing positions, and 9 x 125 km moves
Firing rate demonstrated using 24 volt technology automatic loader
Firing rate 3 rounds in 9.2 seconds
Firing rate 8 rounds in 42.9 seconds
Firing rate 10 rounds in 59.6 seconds
Sustained firing rate 20 rounds in 2 minutes 10 seconds
Firing rate demonstrated using 48 volt technology automatic loader
Firing rate 3 rounds in 8.4 seconds
Firing rate 12 rounds in 59.74 seconds
Sustained firing rate 20 rounds in 1 minute 47 seconds
Dimensions
Hull length 7.9 metres
Overall length 11.7 metres
Barrel overhang 3.3 metres
Width 3.6 metres
Height 3.1 metres
Combat weight 55 tons
Power
Powerpack MTU type 881
Power to weight ratio 13.4 kW/ton
Rating 736 kW
Transmission Renk HSWL 284C
Vehicle performance
Highway speed greater than 60 km/hour
Typical tank cross country speed greater than 45 km/hour
Radius of action 420 kilometres
Transportability STANAG 2832 B
Forward slope 50%
Trench crossing 3 metres
Cost is $5.0Million
MSTA-S 2S19 152MM - SPECIFICATION
152 mm howitzer
Armament
12.7 mm machine gun
Maximum firing range
HEF projectile 24.7 km
HEF gas-assisted projectile 28.5 km
Minimum firing range 6.5 km
Maximum rate of fire 8 rds/min
Elevation +68 to -3 degrees
Traverse 360 degrees
HEF projectile weight 43.56 kg
Onboard ammunition load
152 mm 50 rounds
Machine gun 300 cartridges
Mount weight 42.5 tons
Crew 5
Road speed 60 km/hr
Road range 500 km
Dimensions
Length (gun forwards) 11.91 m
Width 3.3 m
Height (to turret top) 2.98 m
Obstacles
Gradient 47%
Side slope 36%
Trench width 2.8 m
Power-to-weight ratio 18.5 - 20 hp/t
Vertical obstacle 0.5 m
2K25 KRASNOPOL PRECISION-GUIDED MUNITION
Calibre 152 mm
Warhead HE-FRAG
Guidance inertial and semi-active laser homing
First shot fixed target hit probability 0.9
Firing range
Maximum 22 km (from 2S19 MSTA-S)
Minimun 3 km
Range of tank type target (illuminated by 1D22) 7 km
Length 1300 mm
Weight
Projectile 50 kg
Warhead 20.5 kg
Explosive 6.4 kg
Cost is $6.0Million
TIGER - SPECIFICATION
Design mission weight 5400 kilograms
Alternate gross weight 6000 kilograms
Length 14 metres
Height 3.81 metres
Wing span 13 metres
Hover out of ground effect (OGE) 3200 metres, anti-tank version
3500 metres, combat support version
Vertical rate of climb 5.2 metres per sec, anti-tank version
6.4 metres per sec, combat support version
Maximum rate of climb 10.7 metres per sec, anti-tank version
11.5 metres per sec, combat support version
Flight speed, armed 145 knots, anti-tank version
155 knots, combat support version
Cruise speed 124 knots
Design limit speed 161 knots, anti-tank version
174 knots, combat support version
Maximum range, internal fuel 800 km
Mission endurance 2 hours 50 minutes
Maximum endurance, internal fuel 3 hours 25 minutes
Agility 40 degree angle of yaw after first second
Trigat missile range 500 metres to 5 kilometres
Maximum air to air missile range > 5 kilometres Maximum autonomous
Target identification and engagement 5 kilometres
Maximum internal fuel capacity 1020 kilograms
Maximum internal plus external fuel capacity 1575 kilograms
Cost is $15Million
AH-64A/D APACHE - SPECIFICATION
Crew 2 crew: pilot and copilot/gunner
Diameter main rotor blades 14,630 cm
Height 3,590 cm
Empty weight 5,352 kilograms
Maximum cruising speed 260 kilometres per hour
Maximum rate of climb 942 meters per minute
Maximum vertical rate of climb 474 meters per minute
Range 400 kilometres on internal fuel
1,900 kilometres on internal and external fuel
Maximum endurance 3 hours 9 minutes on internal fuel
The g limit values +3.5 g to -0.5 g
Cost is $15million.
AH-1W / AH-1Z SUPER COBRA - SPECIFICATION
Dimensions
Length 13.9 metres
Height 4.02 metres
Rotor diameter 14.63 metres
Powerplant 2 General Electric T700-401 rated at 1,625 shp
Weight
Empty weight 12,200 lbs (10,920 lbs)
Maximum gross weight 16,800 lbs (14,750 lbs)
Internal fuel 2755 lbs(2,086 lbs)
Maximum ordnance 3,914 lbs (1,661 lbs)
Hovering out of ground effect (HOGE) gross weight 16,600 lbs (10,300 lbs)
Performance
Maximum airspeed 210 knots (170 knots)
Cruise speed at altitude 3,000 ft and 91.5 deg F 148 knots (137 knots)
Cruise speed at altitude 4,000 ft and 95 deg F 137 knots (131 knots)
Maximum range with 20 minutes reserve fuel 350 nautical miles
Endurance with 20 minutes reserve fuel 3 hours 30 minutes (2 h 48 min)
Maximum g-load +3.2 g (+2.5g)
Minimum g-load -0.5 g (+0.5g)
Vertical rate of climb at altitude 3,000 ft 1,740 ft/minute (645 ft/minute)
Vertical rate of climb at altitude 4,000 ft 1,386 ft/minute (315 ft/minute)
Vertical rate of climb at altitude 5,000 ft 1,386 ft/minute (315 ft/minute)
Cost is $12Million.
S-70A BLACK HAWK - SPECIFICATION
Dimensions
Main rotor diameter 53 ft 8 inches
Tail rotor diameter 11 ft 0 inches
Overall length with rotors turning 64 ft 9 inches
Maximum height to top turning tail rotor 16ft 9 inches
Width fuselage 7 ft 9 inches
Weights
Empty weight 11,780 lbs
Mission gross weight 16,864 lbs
Maximum gross weight 22,000 Ibs
Engines
Two turboshaft engines General Electric T700-GE-701 C
Power 1,940 shaft horsepower
Transmission rating 3,400 shaft horsepower
Internal fuel 360 US gallons (1,360 litres)
External auxiliary fuel tanks on ESSS system 460 US gallons (1740 litres)
Endurance on internal fuel 3 hours 5 minutes
Maximum endurance with auxiliary fuel 7 hours 21 minutes
Performance
Performance figures at 16,864 lbs Missions Gross Weight:
Maximum Cruise Speed at 5,000 ft 162 kts
VNE (not to exceed speed) 190 kts
Service ceiling 19,000 ft
Hover ceiling, out of ground effect (OGE) 10,600 ft
Maximum range at 5,000 ft 304 nautical miles
Cost is $15Million.
CH-47D/MH-47E CHINOOK - SPECIFICATION
Dimensions
Overall length, rotors turning 30.2 m
Fuselage length 15.6 m
Distance between rotor centres 11.9 m
Width Fuselage 3.8 m
Overall height 5.8 m
Internal length 9.3 m
Internal width 2.3 m
Internal height 2.0 m
Accommodation 3 crew
Troop seats 44
Litters (stretchers) 24
Weight
Empty weight 10,578 kg
Maximum gross weight 24,494 kg
Useful load 13,916 kg
Forward and aft cargo hooks 9,072 kg
Centre cargo hook 12,701 kg
Performance
Sea level cruise speed 265 km/hour
Speed at maximum continuous power 269 km/hour
Rate of climb 464 metres per minute
Service ceiling 2575 m
Hover in ground effect 2,499 m
Hover out of ground effect 1,509 m
Range 426 km
Engines
Model two T55-L-712 SSB
Maximum shaft horsepower 2796 kW
Continuous shaft horse power 2237 kW
Rotor system 2 hubs, 3 blades per hub
Blades fibreglass
Speed 225 rpm
Diameter 18.29 m
Disc area 262.67 square m
Blade folding manual
Cost is $30Million.
T 80U - SPECIFICATION
Crew 3
Weight 46 tons
Engine GTD three shafts with two cascades of turbocompression power turbine and GTD-1250 controlled nozzle assembly
Power 1250 hp
Transmission mechanical, planetary
Track metallic with RMSh and rubber-tyred road wheels
Suspension torsion bar
Shock absorbers hydraulic, telescopic (on 1, 2 and 6 road wheels)
Electrical equipment 22 - 29 V DC
Starter storage batteries 4
Total capacity 340 A h
Radio receive/transmit, telephone, simplex, R-173
Intercom for four men R-174
Ground pressure 0.865 kg/sq cm
Road speed unpaved 40 - 45 km/hour
paved 60 - 65 km/hour
maximum 70 km/hour
Fuel consumption for 100 km
unpaved road 460 - 790 litres
paved road 430 - 500 litres
Fuel endurance
unpaved road 335 km (main fuel tanks)
400 km (with extra fuel drums)
paved road 500 km (main fuel tanks)
600 km (with extra fuel drums)
Negotiable obstacles
gradient 32 deg
side slope 30 deg
trench 2.85 m
Fording depth
without preparation 1.2 m
with preparation 1.8 m
with OVPT snorkel 5 m
Dimensions
length (gun forwards) 944.0Million
H Bombs
small compact
radiation will last for years
comes with a lauch carrirer
or can be used in a silo