Bell 206 JetRanger
Notes: This helicopter was originally sold as the civil equivalent of the OH-58A Kiowa military helicopter, but with improvements, was taken into service as a military helicopter in over 20 countries, primarily as a training helicopter or liaison or observation craft. Unlike the Kiowa, it has no hardpoints and is strictly a cargo helicopter. A JetRanger, fitted with an aerial refueling boom (not standard), was the first helicopter to fly around the world. The JetRanger is reputedly a very easy and forgiving helicopter to fly and has set records for aviation safety. The standard version has no ejection seats and cannot be refueled in air.
The Bell 206A was the first model of the JetRanger. This was superseded by the Bell 206B JetRanger II, with a less powerful but more efficient engine; it is used by the US Navy as a trainer under the designation TH-57B SeaRanger. The Bell 206B-3 JetRanger III was the next version, with a more powerful engine; it is used as a training helicopter by the US Army with the designation TH-67 Creek, and by the US Navy for the same purpose as the TH-57C SeaRanger. The Bell 206L-1 LongRanger was the first stretched version of the JetRanger, based on the JetRanger III. The 206L-2 increased the engine power, and the 206L-3 increases it even further. The Bell 206L-4 is a Canadian built version of the LongRanger; it uses a different engine and avionics.
Finally, the Iranians use a light gunship called the Zafar 300, based on the Bell 206B.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Bell 206A |
$78,872 |
AvG |
680 kg |
1.47 tons |
2+3 |
4 |
None |
Enclosed |
|
Bell 206B |
$78,492 |
AvG |
680 kg |
1.39 tons |
2+3 |
4 |
None |
Enclosed |
|
Bell 206B-3 |
$78,792 |
AvG |
680 kg |
1.45 tons |
2+3 |
4 |
None |
Enclosed |
|
Bell 206L-1 |
$80,008 |
AvG |
907 kg |
1.84 tons |
2+5 or 2 stretchers |
4 |
None |
Enclosed |
|
Bell 206L-2 |
$81,408 |
AvG |
907 kg |
1.86 tons |
2+5 or 2 stretchers |
4 |
None |
Enclosed |
|
Bell 206L-3 |
$83,448 |
AvG |
907 kg |
1.96 tons |
2+5 or 2 stretchers |
4 |
None |
Enclosed |
|
Bell 206L-4 |
$84,558 |
AvG |
1.04 tons |
2.06 tons |
2+5 or 2 stretchers |
4 |
None |
Enclosed |
|
Bell 206LT |
$89,148 |
AvG |
772 kg |
2.01 tons |
2+5 or 2 stretchers |
4 |
None |
Enclosed |
|
Zafar 300 |
$222,590 |
AvG |
680 kg |
1.49 tons |
2+2 |
4 |
Image Intensification |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
Bell 206A |
452 |
113 |
20/28 |
270 |
148 |
4602 |
|
Bell 206B/Zafar 300 |
445 |
111 |
20/28 |
270 |
139 |
4602 |
|
Bell 206B-3 |
450 |
113 |
20/28 |
270 |
146 |
4602 |
|
Bell 206L-1 |
425 |
106 |
20/27 |
270 |
146 |
4602 |
|
Bell 206L-2 |
441 |
110 |
20/28 |
270 |
172 |
4602 |
|
Bell 206L-3 |
447 |
112 |
20/28 |
270 |
260 |
4602 |
|
Bell 206L-4 |
453 |
113 |
20/28 |
270 |
260 |
4602 |
|
Bell 206LT |
482 |
121 |
20/30 |
270 |
375 |
6096 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
(All Others) |
None |
22m |
None |
None |
None |
|
Zafar 300 |
None |
23m |
+2 |
M-134 Minigun, 2 Hardpoints |
1000x7.62mm |
Bell 214A
Notes: The Bell 214 is a development of the Bell "Huey" series was designed for "hot and high" conditions – high altitude and hot weather, where helicopters normally don’t function nearly as well as otherwise. It was first produced for the armed forces of the Shah of Iran. The design features a longer fuselage and more powerful engines. The helicopter has no ejection seats, and is not capable of in-flight refueling.
The Bell 214A Isfahan was the first of the 214 series. These helicopters were taken over by Revolutionary Iran's forces and later built without license. Bell then sold the helicopter to other countries, including Brunei, Columbia, Ecuador, Iraq, Oman, Peru, Philippines, Thailand, the UAE, and Venezuela. At least one captured model of this helicopter is flown by the 82nd Airborne Division's commander in Iran. The Bell 214B BigLifter is a civilian version of the 214A; the 214C is a search and rescue variant with a rescue hoist that has a capacity of 275 kg. The 214ST is a twin engined variant of the Bell 214, normally used by civilians.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Bell 214A |
$284,072 |
AvG |
2.18 tons |
7.48 tons |
2+16 |
10 |
None |
Enclosed |
|
Bell 214B |
$141,548 |
AvG |
2.18 tons |
7.26 tons |
2+16 |
8 |
None |
Enclosed |
|
Bell 214C |
$254,418 |
AvG |
2.18 tons |
7.44 tons |
3+15 |
8 |
None |
Enclosed |
|
Bell 214ST |
$159,468 |
AvG |
2.49 tons |
9.45 tons |
2+16 |
10 |
None |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
Bell 214A/B/C |
522 |
130 |
45/33 |
1647 |
753 |
4500 |
|
Bell 214ST |
576 |
144 |
45/36 |
1647 |
1201 |
4500 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
Bell 214A |
Flare/Chaff Dispensers |
32m |
+1 |
2xM-60E2 Doorguns, 2 Hardpoints |
1200x7.62mm |
|
Bell 214B |
None |
32m |
None |
None |
None |
|
Bell 214C |
Radio Direction Finder, Flare/Chaff Dispensers |
32m |
None |
2xM-60E2 Doorguns |
800x7.62mm |
|
Bell 214ST |
None |
32m |
None |
None |
None |
Bell 412
Notes: This is the latest variant of the UH-1 Huey series. It features the most powerful engines available on a Huey helicopter, and a 4-bladed rotor. It is used by a large number of nations, including countries on all continents except Antarctica. It uses the large sliding doors on either side of all Hueys, and has twin engines.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$186,212 |
AvG |
2.29 tons |
5.4 tons |
2+13 |
8 |
None |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
536 |
134 |
45/33 |
1251 |
660 |
5304 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
None |
30m |
None |
None |
None |
CH-34 Seahorse/Choctaw
Notes: This is the military version of the S-58 helicopter. The CH-34 version is called the Choctaw, while the UH-34 is called the Seahorse. These are very old helicopters that saw their last active US service in Vietnam, but continue to be used in South America and Southeast Asia. They are large and slow helicopters that nonetheless seem to get the job done.
The CH-34 was the first military version, first flown shortly after the Korean War. They were often armed and used as gunships until the advent of gunship versions of the UH-1. The UH-34 was the Marine version of the CH-34, but differed little from the CH-34. The S-58T is a twin-engine development of the civilian S-58, little used by the military.
Westland of Great Britain acquired a license to build the S-58 in 1956; they built a version known as the Wessex. The HC-2 version is a standard sort of utility/cargo helicopter, a counterpart to the CH-34 Choctaw. It uses two British-made engines instead of the one engine of the American version. It can be distinguished by the large exhaust pipe on either side of the nose (the engines are in the nose).
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-34 |
$380,467 |
AvG |
2.77 tons |
6.35 tons |
3+16 or 8 stretchers |
8 |
None |
Enclosed |
|
S-58T |
$285,432 |
AvG |
3.63 tons |
5.9 tons |
3+16 or 8 stretchers |
8 |
None |
Enclosed |
|
HC-2 |
$399,108 |
AvG |
3.63 tons |
6.12 tons |
3+16 or 8 stretchers |
10 |
None |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
CH/UH-34 |
396 |
99 |
85/25 |
615 |
529 |
3000 |
|
S-58T |
444 |
111 |
85/28 |
615 |
654 |
3000 |
|
HC-2 |
452 |
113 |
85/28 |
615 |
961 |
3000 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
CH/UH-34 |
None |
40m |
None |
2xM-60E2 (right door, left rear window), 2 Hardpoints |
2000x7.62mm |
|
S-58T |
None |
40m |
None |
None |
None |
|
HC-2 |
None |
40m |
None |
2xMAG (right door, left rear window), 2 Hardpoints |
2000x7.62mm |
CH-46 Sea Knight
Notes: Also known to the Marines as the Frog, it is also flown by Canada (where it is known as the CH-113), Japan (where it is known as the KV-107), and Sweden (where it is known as the HKP-4). It is often mistaken for the Chinook, but the CH-46 has three wheels instead of the four the Chinook usually has and the Chinook is larger.
The original model is the CH-46A. The SAR version of this helicopter is the HH-46A; it has Doppler search radar and a radio beacon finder, as well as a hoist with a capacity of 300 kg. The next operational transport was the CH-46D, with better engines; the HH-46D is the SAR version of this aircraft, and equipped in a similar manner to the HH-46A. The CH-47E was to be the final version of the Sea Knight (it was to be replaced by the Osprey); it has even more powerful engines. Due to the delays in the Osprey program, the US Marines updated their CH-47Ds and Es with better avionics and some defensive systems.
Twilight 2000 Notes: This helicopter was replaced in US Marines service by the V-22 Osprey series, but many were recalled to service during the Twilight War to replace Osprey losses. The CH-46E and CH-46F do not exist.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-46A |
$185,736 |
AvG |
3.8 tons |
9.71 tons |
3+25 |
14 |
None |
Enclosed |
|
HH-46A |
$373,395 |
AvG |
3.8 tons |
9.71 tons |
3+24 |
16 |
Radar, WL Searchlight |
Enclosed |
|
CH-46D |
$190,216 |
AvG |
4.08 tons |
10.43 tons |
3+25 |
14 |
None |
Enclosed |
|
HH-46D |
$378,233 |
AvG |
4.08 tons |
10.43 tons |
3+24 |
16 |
Radar, WL Searchlight |
Enclosed |
|
CH-46E |
$253,920 |
AvG |
4.08 tons |
10.43 tons |
3+25 |
14 |
None |
Enclosed |
|
CH-46F |
$633,861 |
AvG |
4.08 tons |
10.55 tons |
3+25 |
18 |
None |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
CH-46A/HH-46A |
498 |
125 |
45/31 |
1032 |
918 |
4267 |
|
CH-46D/HH-46D |
505 |
126 |
45/32 |
1032 |
1032 |
4267 |
|
CH-46E/F |
512 |
128 |
45/32 |
1032 |
1382 |
3350 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
CH-46A/D/E |
None |
45m |
None |
2xM-60 Doorguns |
2000x7.62mm |
|
HH-46A/E |
Radio Direction Finder |
45m |
None |
2xM-60 Doorguns |
2000x7.62mm |
|
CH-46F |
Flare/Chaff Dispensers, RWR, LWR, GPS |
45m |
None |
2xM-60 Doorguns |
2000x7.62mm |
CH-47D Chinook
Notes: The CH-47D Chinook is the US armed forces standard medium-lift helicopter and is also found in service with many other nations in both military and civilian versions. There is one door behind the cabin on either side and a rear cargo ramp. The helicopter is capable of water landings without special floatation devices and has an integral hydraulic rescue winch and cargo hooks for slung loads.
The CH-47A was the first model, first used in 1961. This was followed by the increased-capability CH-47B. The CH-47C was the most powerful of the Chinooks, with extra fuel capacity, but it was also quite slow and fuel-hungry and was withdrawn. The CH-47D is the most produced version, and currently the standard US Army version. The CH-47F is the new version, with engines that function better in "hot and high" environments. They have improved avionics and survivability. The CH-47SD (Super-D) is a modernization of the CH-47D with radar and considerable defensive avionics.
Twilight 2000 Notes: The CH-47F is a rare variant, and the CH-47SD does not exist.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-47A |
$658,674 |
AvG |
10.21 tons (up to 5.76 tons internal) |
20.24 tons |
3+33 or 25 paratroops or 18 stretchers |
22 |
None |
Enclosed |
|
CH-47B |
$685,391 |
AvG |
13.22 tons (up to 7.46 tons internal) |
24.99 tons |
3+44 or 33 paratroops or 24 stretchers |
26 |
None |
Enclosed |
|
CH-47C |
$722,430 |
AvG |
15.56 tons (up to 8.78 tons internal) |
27.93 tons |
3+44 or 33 paratroops or 24 stretchers |
30 |
None |
Enclosed |
|
CH-47D |
$920,899 |
AvG |
13.92 tons (up to 7.85 tons internal) |
24.49 tons |
3+44 or 33 paratroops or 24 stretchers |
28 |
None |
Enclosed |
|
CH-47F |
$1,239,172 |
AvG |
13.92 tons (up to 7.85 tons internal) |
22.68 tons |
3+44 or 33 paratroops or 24 stretchers |
32 |
None |
Enclosed |
|
CH-47SD |
$1,985,682 |
AvG |
12.94 tons (up to 7.3 tons internal) |
24.49 tons |
3+44 or 33 paratroops or 24 stretchers |
34 |
Radar |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
CH-47A |
418 |
105 |
60/26 |
3900 |
1623 |
2575 |
|
CH-47B |
531 |
133 |
60/33 |
3900 |
2107 |
2575 |
|
CH-47C |
482 |
121 |
65/30 |
3900 |
2778 |
2575 |
|
CH-47D |
538 |
135 |
60/34 |
4200 |
2219 |
2575 |
|
CH-47F |
589 |
147 |
60/37 |
3900 |
3610 |
4800 |
|
CH-47SD |
574 |
144 |
55/36 |
7828 |
3390 |
3383 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
CH-47A/B/C |
None |
80m |
None |
3xM-60 (2xright side door, 1xleft side window) |
3000x7.62mm |
|
CH-47D |
Flare/Chaff Dispensers |
80m |
None |
3xM-60 (2xright side door, 1xleft side window) |
3000x7.62mm |
|
CH-47F |
Flare/Chaff Dispensers (32), Secure Radios, RWR |
80m |
None |
3xM-60 (2xright side door, 1xleft side window) |
3000x7.62mm |
|
CH-47SD |
Flare/Chaff Dispensers (32), Secure Radios, RWR, LWR, ECM, Armored Cockpit |
80m |
None |
3xM-60 (2xright side door, 1xleft side window) |
3000x7.62mm |
CH-53 Sea Stallion
Notes: This helicopter is used as a medium lift helicopter by the US Marines, though it has been largely supplanted by the CH-53E Super Stallion. It is also in use by other armed forces worldwide. It has a rear ramp and a side door. Optionally, twin drop tanks may be carried for an extra 3406 liters of fuel. It is capable of amphibious landings.
The CH-53A was the first model, first flown in 1964. Its hardpoints may only be used for drop tanks. The HH-53B, also known as the Super Jolly, is a search and rescue variant used by the USAF, with a rescue hoist that has a capacity of 272 kg, and equipment to aid its searches. It also has a probe for aerial refueling, and jettisonable extra fuel tanks. The engines are not as powerful as those on the CH-53A, but this further extends range. The HH-53C brings more powerful engines back. The CH-53D is a further improvement of the CH-53A, with more powerful engines. The Ya’sur 2000 is the result of an Israeli modernization program for the CH-53D; it is estimated to have extended the life of the CH-53D in Israeli service by 20 years.
Twilight 2000 Notes: The Ya’sur 2000 does not exist, but the Israelis did acquire some extra CH-53E Super Stallions instead.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-53A |
$868,095 |
AvG |
5.9 tons |
19.05 tons |
3+37 or 28 paratroops or 24 stretchers |
26 |
None |
Enclosed |
|
HH-53B |
$1,187,093 |
AvG |
5.9 tons |
19.05 tons |
3+37 |
26 |
None |
Enclosed |
|
HH-53C |
$1,246,323 |
AvG |
5.9 tons |
19.05 tons |
3+37 |
28 |
None |
Enclosed |
|
CH-53D |
$1,559,779 |
AvG |
5.9 tons |
19.05 tons |
3+37 or 28 paratroops or 24 stretchers |
28 |
None |
Enclosed |
|
Ya’sur 2000 |
$2,519,548 |
AvG |
5.9 tons |
19.05 tons |
3+37 or 28 paratroops or 24 stretchers |
28 |
Weather Radar |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
CH-53A |
628 |
157 |
55/39 |
4500 |
2549 |
3400 |
|
HH-53B |
611 |
153 |
55/38 |
7906 |
2279 |
3400 |
|
HH-53C |
649 |
162 |
55/41 |
7906 |
2909 |
3400 |
|
CH-53D/Ya’sur 2000 |
653 |
163 |
55/41 |
4500 |
2914 |
3795 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
CH-53A |
None |
40m |
None |
2xM-2HB (Rear, Left Side Door), 2 Hardpoints |
1500x.50 |
|
HH-53B/C |
Radio Direction Finder |
40m |
None |
2xM-2HB (Rear, Left Side Door) |
1500x.50 |
|
CH-53D |
Armored Cockpit, Flare/Chaff Dispensers |
50m |
None |
2xM-2HB (Rear, Left Side Door), 2 Hardpoints |
1500x.50 |
|
Ya’sur 2000 |
Armored Cockpit, Flare/Chaff Dispensers, RWR, GPS |
50m |
None |
2xM-2HB (Rear, Left Side Door), 2 Hardpoints |
1500x.50 |
CH-53E Super Stallion
Notes: This is a stretched and up-engined version of the Sea Stallion. The Super Stallion has a total of three engines for superior lifting capability. The Super Stallion also has a rear ramp, but has two side doors, each with a door gun. Optionally, twin drop tanks may be carried for an extra 4290 liters of fuel, and may also carry an internal extra fuel tank for an additional 8265 liters of fuel. The Super Stallion is capable of in-flight refueling and buddy refueling, and is capable of amphibious landings. It may be noted that while US Super Stallions normally mount only drop tanks on the hardpoints, the Israelis regularly mount weapons.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$3,548,199 |
AvG |
16.33 tons (up to 13.26 tons internal) |
33.34 tons |
3+55 |
42 |
Weather Radar |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
630 |
157 |
55/39 |
8619 |
5865 |
4000 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
Armored Cockpit, Flare/Chaff Dispensers, IRCM, RWR |
40m |
None |
3xM-2HB (Right, Left, Rear), 2 Hardpoints |
2250x.50 |
CH-54 Tarhe
Notes: This heavy-lift helicopter is in both military and civilian use (and known as the Skycrane in its civilian guise). It normally uses an external cargo pod, but also has a lifting winch. The Tarhe has long landing gear that enables it to straddle and lift its cargo. Normal cargo pods are 9-ton capacity pods that contain mobile hospitals, command posts, barracks, and other special loads. A common use in Vietnam was to retrieve crash-landed aircraft. The third crewmember is a loadmaster that faces rearward to direct loading and winching operations.
Twilight 2000 Notes: Most stocks of Tarhes were relegated to Reserve status before the Twilight War, but many were reactivated as the war intensified.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-54A |
$291,568 |
AvG |
300 kg internal, plus 8.78 tons external |
19.05 tons |
3+Special (up to 45 or 24 stretchers in pod) |
28 |
None |
Enclosed |
|
CH-54B |
$300,508 |
AvG |
300 kg internal, plus 9.07 tons external |
21.32 tons |
3+Special (up to 45 or 24 stretchers in pod) |
30 |
None |
Enclosed |
|
CH-54E |
$388,588 |
AvG |
300 kg internal, plus 12.5 tons external |
24.75 tons |
3+Special (up to 90 or 48 stretchers in pod) |
58 |
None |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
CH-54A |
346 |
86 |
80/22 |
4350 |
3343 |
4000 |
|
CH-54B |
338 |
85 |
80/21 |
4350 |
3567 |
4000 |
|
CH-54E |
301 |
75 |
80/19 |
4350 |
3269 |
4000 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
(All) |
None |
55m |
None |
None |
None |
H-13/UH-13 Sioux
Notes: This light helicopter was one of the first service helicopters anywhere in the world, first built in 1943. It's most famous use is as a medivac in the Korean War, often seen in the TV series MASH. It is still used as a liaison and observation helicopter by some Third World countries, but is most often found in civil use or as restored aircraft flown by private civilian operators. It is a light aircraft with a limited payload. The UH-13 is longer with extra seats.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
H-13 |
$40,318 |
AvG |
240 kg |
1.34 tons |
2+1 |
4 |
None |
Open |
|
UH-13 |
$40,518 |
AvG |
300 kg |
1.73 tons |
2+2 |
4 |
None |
Open |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
H-13 |
340 |
85 |
30/21 |
170 |
99 |
5394 |
|
UH-13 |
338 |
85 |
30/21 |
170 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
(Both) |
None |
25m |
None |
None |
None |
HH-3E Jolly Green Giant
Notes: This is a large cargo helicopter used by Italy and formerly used by the US Air Force and Army for large combat operations and loads. (In US service, it has been largely replaced by the CH-53.) The Jolly Green Giant is heavily armored and armed. It has a rear ramp, a door on the starboard side behind the cockpit, and 450-kg capacity winch on the side door. The Jolly Green is still used by the US Coast Guard (where it is known as the Pelican), as it is capable of amphibious landings. The Jolly Green has no ejection seats, but is capable of in-flight refueling.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$833,445 |
AvG |
4.8 tons (up to 2.25 tons internal) |
9.92 tons |
4+25 or 15 stretchers |
16 |
None |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
525 |
131 |
40/33 |
2880 |
1106 |
3636 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
Flare/Chaff Dispensers, Armored Cockpit, INS |
50m |
None |
M-2HB (Right Door), M-2HB (Rear), 2 Hardpoints |
2000x.50 |
OH-6 Cayuse
Notes: This light observation helicopter was replaced in active US Army service by the OH-58, but is still used in Reserve and National Guard service and in many other countries. Countries using it include Argentina, Chile, Columbia, Mexico, Philippines, and Vietnam. Is US service it is usually known as the Loach (for the initials of Light Observation/Cargo Helicopter, LOCH).
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
OH-6A |
$316,687 |
AvG |
455 kg |
1.09 tons |
2+2 |
4 |
None |
Enclosed |
|
OH-6B |
$702,074 |
AvG |
520 kg |
1.49 tons |
2+2 |
4 |
FLIR |
Enclosed |
|
OH-6D |
$702,598 |
AvG |
525 kg |
1.57 tons |
2+2 |
4 |
FLIR |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
OH-6A |
480 |
120 |
20/30 |
340 |
44 |
4380 |
|
OH-6B |
546 |
136 |
20/34 |
340 |
105 |
4380 |
|
OH-6D |
553 |
138 |
20/35 |
340 |
116 |
4380 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
(All) |
Flare/Chaff Dispensers |
24m |
+1 |
2 Hardpoints |
None |
OH-58 Kiowa/Kiowa Warrior
Notes: This is the original version of the Kiowa, first being used by the US Army in Vietnam in 1969. It is normally used as a scout helicopter, and by the 2000 was still being used by Austria, Australia, and Canada, and could still be found in many US Army National Guard units.
The OH-58A was first fielded in 1969. It was used to find targets for AH-1 Cobra gunships and to scout landing zones. One of the weapons first mounted to the Kiowa was the M-134 Minigun, but it was found that the vibration was too great and this practice stopped. In the late 1990s, the OH-58A was retrofitted with a GPS system.
The OH-58C has much more powerful engines. It is also fitted with non-reflective flat glass panels instead of the curved window sections of the OH-58A. In addition to being retrofitted with GPS, some OH-58Cs were also retrofitted with launchers for Stinger missiles.
The OH-58C is based on the Bell 406 airframe. It is fitted with an extensive sensor suite to allow it to work with Apache attack helicopters. The standard OH-58D was later fitted with a mast-mounted sight under the Armed Helicopter Improvement Program (AHIP), to allow it to spot and track targets while hiding behind terrain. The OH-58D is known as the Kiowa Warrior, due to its weapons fit.
The MH-58D is a Saudi version of the OH-58D; it has a 20mm autocannon under the belly, but no mast-mounted sight.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
OH-58A |
$456,632 |
AvG |
345 kg |
1.36 tons |
2+3 |
4 |
Image Intensification |
Enclosed |
|
OH-58C |
$458,404 |
AvG |
397 kg |
1.62 tons |
2+3 |
4 |
Image Intensification |
Enclosed |
|
OH-58D |
$990,967 |
AvG |
907 kg |
2.5 tons |
2 |
6 |
FLIR, Image Intensification |
Enclosed |
|
OH-58D AHIP |
$1,294,898 |
AvG |
907 kg |
2.5 tons |
2 |
8 |
Radar, FLIR, Image Intensification |
Enclosed |
|
MH-58D |
$1,073,485 |
AvG |
907 kg |
2.56 tons |
2 |
6 |
FLIR, Image Intensification |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
OH-58A |
444 |
111 |
15/28 |
185 |
103 |
3500 |
|
OH-58C |
475 |
119 |
15/30 |
185 |
141 |
3500 |
|
OH-58D/AHIP |
474 |
119 |
15/30 |
305 |
186 |
3500 |
|
MH-58D |
469 |
117 |
15/29 |
305 |
186 |
3500 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
OH-58A/C |
Flare/Chaff Dispensers |
36m |
+1 |
2 Hardpoints |
None |
|
OH-58D |
Flare/Chaff Dispensers, IR Suppression, Laser Designator, RWR, Datalink |
38m |
+3 |
2 Hardpoints |
None |
|
OH-58D AHIP |
Flare/Chaff Dispensers, IR Suppression, Laser Designator, Datalink, RWR, LWR, IRCM |
38m |
+3 |
2 Hardpoints |
None |
|
MH-58D |
Flare/Chaff Dispensers, IR Suppression, Laser Designator, RWR, Datalink |
38m |
+3 |
20mm GIAT M-621 Autocannon, 2 Hardpoints |
250x20mm |
S-76 Spirit/Eagle
Notes: This was a private venture by Sikorsky, incorporating technology from the company’s S-70 Blackhawk. The Spirit was directed at both the civilian and military markets, but found most of its sales in the civilian market.
The original S-76 was developed in the late 1970s. The S-76 Mk II is a version with improved avionics. It has an external cargo hook for sling loads. The S-76A has uprated engines, and the S-76B has even more powerful engines.
The AUH-76 is an armed assault helicopter version of the S-76 Mk II. It is known as the Eagle, as are all military models. It has equipment necessary to turn it into an assault craft, including gunsights, hardpoints, and defensive equipment, and miniaturization makes it light. The H-76B is a basic military transport version of the S-76B.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
S-76/S-76 Mk II |
$284,012 |
AvG |
1.07 tons |
4.67 tons |
2+12 |
8 |
None |
Enclosed |
|
S-76A |
$286,172 |
AvG |
1.2 tons |
5.04 tons |
2+12 |
8 |
None |
Enclosed |
|
S-76B |
$418,276 |
AvG |
1.61 tons |
5.31 tons |
2+14 |
8 |
None |
Enclosed |
|
AUH-76 |
$1,679,429 |
AvG |
1.28 tons |
4.46 tons |
2+12 |
16 |
Image Intensification, FLIR |
Enclosed |
|
H-76B |
$1,201,216 |
AvG |
1.61 tons |
5.31 tons |
2+12 |
12 |
Image Intensification, FLIR |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
S-76/S-76 Mk II/AUH-76 |
538 |
135 |
40/34 |
1080 |
429 |
4572 |
|
S-76A |
549 |
137 |
40/34 |
1080 |
483 |
4572 |
|
S-76B/H-76B |
574 |
144 |
40/36 |
1080 |
674 |
4572 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
S-76/Mk II/A/B/C |
None |
40m |
None |
None |
None |
|
AUH-76 |
Secure Radios, Chaff/Flare Dispensers, Armored Cockpit, RWR, LWR, GPS, Laser Designator |
40m |
+3 |
2xM-60E2 Doorguns, 4 Hardpoints, 2 AAM Hardpoints |
1000x7.62mm |
|
H-76B |
Flare/Chaff Dispensers, Armored Cockpit |
40m |
+2 |
2xM-60E2 Doorguns, 4 Hardpoints |
1000x7.62mm |
SH-2 Seasprite
Notes: The Seasprite is known by the US Navy as a LAMPS (Light Airborne Multi-Purpose System) helicopter. It is used for liaison duties and for ASW and search and rescue duties. The Seasprite is normally armed with only anti-ship weapons or none at all, but may be armed with a single M-60E2 doorgun, with a gunner carried at the expense of a passenger. No ejection seats are provided, and the aircraft is not capable of in-flight refueling. The Seasprite is used by the US Navy (put back in production in 1981), Australia, Egypt, Taiwan, and New Zealand.
The UH-2B is the standard utility version, used to transport personnel and cargo back and forth from ships. It is not normally used as an assault transport. This is the version detailed below.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
AvG |
1.81 tons |
6.08 tons |
3+8 |
8 |
None |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
554 |
139 |
50/35 |
1800 |
1062 |
3075 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
None |
45m |
None |
M-60E2, 2 hardpoints |
500x7.62mm |
SH-3H Sea King
Notes: The first SH-3 made its first flight in 1959, and since then they have been steadily upgraded. It is used throughout the US Navy and NATO service, as well as Argentina, Australia, Brazil, Egypt, India, Iraq, Iran, Japan, Pakistan, Peru, Qatar, Saudi Arabia, Thailand, and Venezuela. It is primarily used for transport and liaison duties, and is seldom armed. A door gun can be fitted and a gunner carried at the expense of one passenger. ASW and search and rescue variants also exist. A version of this helicopter, known as the V-3D, functions as a presidential transport (Marine One and Two).
The various antisubmarine/antishipping versions will not be detailed here. The utility versions include the UH-3A, a cargo helicopter modified from the SH-3A; the HH-3B, a UH-3A with upgraded avionics, and the UH-3H, a fully modernized version of the UH-3. The HH-3A is a combat SAR version of the CH-3A. It has various improvements to allow it to find and rescue downed aircrew and survivors of sunken ships, and protect them if necessary, including a rescue hoist with a capacity of 272 kg. The British counterpart is the Sea King HAR.5; it is basically similar for game purposes, but has different armament and different engines.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
CH-3A |
$500,283 |
AvG |
3.44 tons |
8.63 tons |
3+26 |
14 |
None |
Enclosed |
|
HH-3A |
$2,215,494 |
AvG |
3.44 tons |
9.18 tons |
3+15 |
18 |
Radar |
Enclosed |
|
UH-3H |
$604,359 |
AvG |
3.63 tons |
9.53 tons |
3+26 |
14 |
None |
Enclosed |
|
HAR.5 |
$2,222,087 |
AvG |
3.63 tons |
9.75 tons |
3+15 |
18 |
Radar |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
UH-3A/B/HH-3A |
506 |
126 |
60/32 |
2800 |
460 |
3000 |
|
UH-3H |
534 |
134 |
60/33 |
2800 |
513 |
3000 |
|
HAR.5 |
537 |
134 |
60/34 |
2800 |
487 |
3000 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
UH-3A/B |
None |
40m |
None |
M-60E2 Doorgun, 2 Hardpoints |
1000x7.62mm |
|
HH-3A |
Flare/Chaff Dispensers, Radio Direction Finder, RWR |
40m |
+2 |
M-134 Minigun, 2 Hardpoints |
2000x7.62mm |
|
UH-3H |
Flare/Chaff Dispensers |
40m |
+1 |
M-60E2 Doorgun, 2 Hardpoints |
1000x7.62mm |
|
HAR.5 |
Flare/Chaff Dispensers, Radio Direction Finder, RWR |
40m |
+2 |
MAG Doorgun, 2 Hardpoints |
2000x7.62mm |
TH-55/H-55 Osage
Notes: This light helicopter was used until the as the US Army's basic training helicopter until the early 1980s, when it was replaced by the UH-1H Iroquois. With large numbers of the UH-1H taken back into service as troop transport helicopters during the Twilight War, the TH-55 was brought back as a training helicopter. Later, they were used in the United States as light observation and artillery spotting helicopters. It is a simple, light, no-frills helicopter that is easy to maintain, simple to fly, and cheap to operate. The H-55 version is used as a utility helicopter or training helicopter by Algeria, Brazil, Colombia, Ghana, Haiti, Japan, Kenya, Nicaragua, Sierra Leone, Spain, and Sweden, and is also in wide use by civilian operators and police departments worldwide.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$73,588 |
AvG |
267 kg |
725 kg |
2 |
None |
Open |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
276 |
69 |
20/17 |
125 |
62 |
3625 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
None |
16m |
None |
None |
None |
UH-1 Iroquois
Notes: The famous "Huey" (the nickname based on its original US Army designation, the HU-1A) has seen action in conflicts all over the globe, including its most famous use by the US in Vietnam. It still serves to this day with the US Marines, who consider the UH-1N and UH-1Y to be better than the Blackhawk, as well as scores of countries worldwide, not to mention thousands of civilian operators. It is perhaps the most common helicopter in the world today.
The UH-1A was the original US Army version, based on the Bell 204 airframe. The UH-1B has a better seating arrangement to allow one more passenger. The UH-1C is improved with a more powerful engine. It was often used as a gunship, loaded with guns and rocket pods, before the advent of the Cobra. The UH-1E is a version for the USMC with a 272-kg capacity rescue hoist and a chin turret mounting two machineguns. The UH-1F is a version built for the USAF to patrol missile silos; it has a more powerful engine and some surveillance equipment. The HH-1K is a US Navy SARbird, with a rescue hoist with a capacity of 272 kg and limited additional sensors, as well as more powerful engines. The UH-1L is the US Navy utility version of the HH-1K. The UH-1M is a UH-1C with night vision equipment fitted.
The UH-1D is based on the Bell 205 airframe. It is enlarged and has more powerful engines than its predecessor. The UH-1H is a UH-1D with better engines. The HH-1H is a SAR version of the UH-1H, similar in concept to the HH-1K.
The UH-1N is based on the Bell 212 airframe, and is sometimes called the Twin Huey because of the two engines that power it. It is further stretched over the UH-1D.
The US Marines have been upgrading their UH-1Ns to the UH-1Y standard. The UH-1Y has four rotor blades for more agility and lifting ability, a glass cockpit, a computerized flight management system, and defensive capabilities that the previous versions of the UH-1 lacked.
Twilight 2000 Notes: The UH-1Y does not exist.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
UH-1A |
$199,775 |
AvG |
1.18 tons |
3.6 tons |
2+6 |
4 |
None |
Enclosed |
|
UH-1B |
$199,775 |
AvG |
1.18 tons |
3.6 tons |
2+7 |
4 |
None |
Enclosed |
|
UH-1C |
$204,202 |
AvG |
1.36 tons |
4.31 tons |
2+7 |
6 |
None |
Enclosed |
|
UH-1D |
$243,048 |
AvG |
1.56 tons |
3.94 tons |
2+12 |
6 |
None |
Enclosed |
|
UH-1E |
$299,069 |
AvG |
1.36 tons |
4.39 tons |
2+7 |
6 |
None |
Enclosed |
|
UH-1F |
$345,509 |
AvG |
1.36 tons |
4.6 tons |
2+7 |
7 |
Image Intensification |
Enclosed |
|
UH-1H |
$247,886 |
AvG |
1.76 tons |
4.31 tons |
2+12 |
6 |
None |
Enclosed |
|
UH-1L |
$209,040 |
AvG |
1.53 tons |
4.68 tons |
2+7 |
6 |
None |
Enclosed |
|
UH-1M |
$342,442 |
AvG |
1.36 tons |
4.34 tons |
2+7 |
7 |
Passive IR |
Enclosed |
|
UH-1N |
$267,430 |
AvG |
2.27 tons |
5.08 tons |
2+14 |
8 |
None |
Enclosed |
|
UH-1Y |
$599,103 |
AvG |
3.02 tons |
8.39 tons |
2+18 |
12 |
None |
Enclosed |
|
HH-1H |
$558,926 |
AvG |
1.76 tons |
4.34 tons |
2+10 |
8 |
Image Intensification |
Enclosed |
|
HH-1K |
$539,343 |
AvG |
1.53 tons |
4.71 tons |
3+6 |
8 |
Image Intensification |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
UH-1A/B |
180 |
245 |
50/70 |
650 |
305 |
3600 |
|
UH-1C/E/M |
478 |
119 |
50/30 |
650 |
405 |
3505 |
|
UH-1D |
362 |
91 |
50/23 |
945 |
404 |
3840 |
|
UH-1F |
500 |
125 |
50/31 |
650 |
475 |
3505 |
|
UH-1H/HH-1H |
408 |
102 |
50/26 |
945 |
516 |
3840 |
|
UH-1L/HH-1K |
513 |
128 |
50/32 |
650 |
511 |
3505 |
|
UH-1N |
453 |
113 |
50/28 |
815 |
511 |
5273 |
|
UH-1Y |
608 |
152 |
40/38 |
1438 |
1350 |
6100 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
UH-1A/B/C/F/L/M/N |
None |
34m |
None |
2xM-60 Doorguns, 2 Hardpoints |
1000x7.62mm |
|
UH-1E |
None |
34m |
+1 |
2xM-60, 2xM-60 Doorguns, 2 Hardpoints |
2000x7.62mm |
|
HH-1K/H |
Secure Radios, Radio Direction Finder |
34m |
None |
2xM-60 Doorguns, 2 Hardpoints |
1000x7.62mm |
|
UH-1Y |
Secure Radios, Flare/Chaff Dispensers, IR Suppression, RWR, LWR, Armored Cockpit, GPS |
40m |
+2 |
2xMAG Doorguns, 2 Hardpoints |
2000x7.62mm |
UH-60 Blackhawk
Notes: The UH-60 is the US military's primary troop transport and assault helicopter, and is also used by Australia, Bahrain, Brazil, China, Egypt, Israel, Greece, Japan, Jordan, and Mexico. It replaced the UH-1 in the service of most of those countries, bringing improvements in cargo carrying, crashworthiness, and maneuverability. The Blackhawk has no ejection seats, and is not capable on in-flight refueling.
The UH-60L version of the Blackhawk was designed for airmobile assaults, with uprated engines and an improved gearbox for improved lifting capability. The UH-60L has an improved cargo hook with the capability to sling load a HMMWV or light howitzer or a similar weight item. Israeli UH-60Ls have an aerial refueling probe.
The HH-60J Jayhawk is a rescue version of the SH-60B Seahawk, used by the US Navy and Coast Guard. It has a 270kg rescue winch with 60m of cable. Like the SH-60B, it uses different engines, and it also has an aerial refueling probe.
The rarest variant of the Blackhawk is the VH-60N. Originally known as the VH-60A, they were redesignated to avoid confusion with the UH-60A. These helicopters are flown only by the US Marines and are used to fly the President of the United States and other VIPs important to the US on short-range flights where larger helicopters would not be necessary or expedient. Only nine of these variants exist. They start out as standard UH-60As, but (and most of the modifications are classified), have upgraded engines, a powerful communications suite, with a communications officer’s position; EMP protection, biological/chemical warfare protection, a small weather radar on a chin mount, exhaust shields to protect against IR-guided missiles, a soundproofed, luxury cabin, and some minor ECM and IRCM protection. The helicopter carrying the president always carries the call sign of Marine One; if carrying the Vice-President, it will carry the call sign of Marine Two. If other VIPs are carried and the President or Vice-President are not aboard, it receives a randomly-generated call sign. These are the only Blackhawks flown by the US Marines, and they are generally known as "Presidential Hawks."
The SH-60B Seahawk is a Naval LAMPS (Light Airborne Multipurpose System) helicopter, which means that it is designed to perform a variety of roles; in this case, the Seahawk performs roles ranging from cargo and personnel transport to antisubmarine warfare. The Seahawk was designed to replace the old Seasprite LAMPS I and LAMPS II helicopters, and is designated a LAMPS II platform. The SH-60B differs greatly from the UH-60A from which it is derived; the Seahawk has an extensive avionics suite used for the detection and fighting of enemy submarines and a secondary search-and-rescue role. The UH-60A and SH-60B have 83% parts commonality; however, the airframe and exposed parts of the Seahawk are treated to resist salt-water corrosion. The SH-60B features a RAST (Recovery Assist Secure and Traverse) system; this allows the Seahawk to literally "hook" a certain part of the landing pads of ships and then be reeled in, making recovery aboard small ships and in bad weather possible. The rotors, tailfin, horizontal stabilator, and torque rotor all fold to facilitate storage in small spaces. (The stabilator is also rectangular instead of swept as on the UH-60A.) The seats for the crew of the Seahawk are not armored, as on the Blackhawk, though the cabin doors can be jettisoned with explosive bolts. The communications are long-range and secure. The Seahawk has a very efficient autopilot, allowing the aircraft even to hover while maintaining altitude, attitude, and position automatically. The Seahawk is air conditioned, not for the benefit of the crew, but for the avionics suite. Fuel capacity is increased, and the Seahawk has a HIFS (Hover In-Flight System) allows the Seahawk to over above or alongside a ship and be refueled. The Seahawk has a powerful radar in a chin mount; this radar is able to look 360 degrees around the aircraft. The Seahawk has a MAD system to assist in locating and identifying submarines and surface ships. It may be extended on a short boom or towed up to 25 meters behind the Seahawk. The Seahawk has sonobuoy tubes. The SH-60B routinely uses the optional stub wings which can be mounted on either side of all Blackhawk-series helicopters, and generally carries weapons on them, though drop tanks or ECM/IRCM pods may also be carried. Original SH-60Bs had the same engines as the UH-60A, but these were later changed for uprated engines. The Seahawk may also be distinguished by the landing gear; the tail gear is moved to the rear of the fuselage instead of being on the tail boom, and has two wheels instead of one. This also facilitates landing on small landing pads. The landing gear is also taller than the standard Blackhawk.
After 1987, Seahawks were further upgraded, being equipped with a laser jammer similar to that of the Stingray Bradley (see US Tracked Armored Personnel Carriers), flare and chaff dispensers, a radar warning system to alert the crew of missile launches and approaches, door guns, FLIR, and stabilized binoculars. Shortly before the 1991 Gulf War, Block I upgrades were begun, equipping the Seahawk with GPS, a more powerful computer, provision for a GECAL .50 caliber Gatling gun, and upgrades in possible weapons carried to include antishipping missiles and better torpedoes. The left winglet was also extended to include one more hardpoint. (The right side winglet could not be extended, since the stores would get in the way of the rescue hoist.
The SH-60F Ocean Hawk may be thought of as a "stripped" version of the late (though not the Block I) SH-60B; it is designed primarily for "Angel" service (rescuing those aviators who have to ditch soon after takeoff or landing), but may also be used for general SAR service and close-in antisubmarine and antishipping duties. The Ocean Hawk deletes the RAST gear, since it is not required to land on the pads of small ships, and the LAMPS III suite is replaced with a less sophisticated suite. It adds a dipping sonar, but the sonobuoy launchers are removed, replaced by a single sonobuoy launcher with 8 sonobuoys in a rack and the launcher loaded manually. The left winglet is extended to include one more hardpoint, but as the Ocean Hawk retains the SAR hoist, the right winglet is not extended. The Ocean Hawk also has a sling hook under the fuselage to allow it to transport cargo; this hook is able to hoist up to the maximum cargo capacity of the SH-60F. The SH-60F went into service just before the 1991 Gulf War.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
UH-60A |
$463,832 |
AvG |
3.63 tons |
9.19 tons |
3+14 |
12 |
None |
Enclosed |
|
UH-60L |
$604,339 |
AvG |
4.39 tons |
11.11 tons |
3+14 |
14 |
None |
Enclosed |
|
HH-60J |
$992,516 |
AvG |
3.92 tons |
9.93 tons |
3+14 |
18 |
FLIR, Image Intensification |
Enclosed |
|
VH-60N |
$1,282,030 |
AvG |
3 tons |
10 tons |
3+6 |
24 |
FLIR, Radar (Weather) |
Shielded |
|
SH-60B (Early) |
$1,424,720 |
AvG |
3.74 kg |
9.93 kg |
3+6 |
24 |
Radar |
Enclosed |
|
SH-60B (Late) |
$1,854,730 |
AvG |
3.74 kg |
10.51 tons |
3+6 |
24 |
FLIR, Radar, Image Intensifier |
Enclosed |
|
SH-60B (Block I) |
$1,904,730 |
AvG |
3.74 kg |
10.57 tons |
3+6 |
24 |
FLIR, Radar, Image Intensifier |
Enclosed |
|
SH-60F |
$1,538,888 |
AvG |
3.74 tons |
9.42 tons |
3+9 |
20 |
Radar |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
UH-60A |
592 |
148 |
40/37 |
3500 |
1198 |
4000 |
|
UH-60L |
589 |
147 |
40/37 |
3500 |
1435 |
4000 |
|
HH-60J |
604 |
151 |
40/38 |
3500 |
1350 |
4000 |
|
VH-60N |
586 |
147 |
40/38 |
3500 |
1350 |
4000 |
|
SH-60B (Early) |
518 |
130 |
40/37 |
3800 |
1217 |
4000 |
|
SH-60B (Late/Block I) |
525 |
132 |
40/37 |
3800 |
1350 |
4000 |
|
SH-60F |
604 |
151 |
40/37 |
3800 |
1350 |
4000 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
UH-60A |
IR Suppression, Flare/Chaff Dispensers, RWR, GPS |
40m |
None |
2xMAG Doorguns |
2000x7.62mm |
|
UH-60L |
IR Suppression, Flare/Chaff Dispensers, RWR, GPS, IRCM |
40m |
None |
2xMAG Doorguns |
2000x7.62mm |
|
HH-60J |
Secure Radios, IR Suppression, Flare/Chaff Dispensers, RWR, GPS, IRCM |
40m |
None |
2xMAG Doorguns |
2000x7.62mm |
|
VH-60N |
IR Suppression, Flare/Chaff Dispensers. RWR. GPS, ECM, IRCM, Secure Radios, Satcom Radio, Short-Range Radio Jammer |
40m |
None |
None |
None |
|
SH-60B (Early) |
IR Suppression, MAD Sensor, Look-Down Radar, Sonobuoys (125), Inertial Navigation, Secure Radios |
40m |
+2 |
4 Hardpoints |
None |
|
SH-60B (Late) |
IR Suppression, MAD Sensor, Look-Down Radar, Sonobuoys (125), Inertial Navigation, Secure Radios, Laser Jammer, Flare/Chaff Dispensers, RWR |
40m |
+2 |
4 Hardpoints, 2xM-60D Doorguns |
2000x7.62mm |
|
SH-60B (Block I) |
IR Suppression, MAD Sensor, Look-Down Radar, Sonobuoys (125), Inertial Navigation, Secure Radios, Laser Jammer, Flare/Chaff Dispensers, RWR, GPS |
40m |
+3 |
5 Hardpoints, 2xM-60D Doorguns, GAU-19/A |
1000x7.62mm, 500x.50 |
|
SH-60F |
IR Suppression, Dipping Sonar, Sonobuoys (8), Inertial Navigation, Secure Radios, RWR |
40m |
+1 |
5 Hardpoints, 2xM-60D Doorguns |
2000x7.62mm |