![]()
MILNET Brief Army Helicopter Brief: Can the DoD Recover From Its Mistakes "You can't get one commander in Iraq to let one helicopter come home...Fixed-wings (jets) are great, ... but can they get down and do the rooting in a low level in the cities? Can they see down the alleyways? Right now they can't." - Brig. Gen. E. J. Sinclair, commandant of the U.S. Army Aviation Center at Fort Rucker, Alabama. 1 |

| Crew: | 2 |
| Max gross weight: | 5,500 lbs (armed) |
| Empty weight: | 3,289 lbs |
| Height: | 12 ft, 10.6 in |
| Width: | 6 ft, 5.4 in |
| Length: | 33 ft, 4 in |
| Rotor diameter: | 35 ft |
| Max cruise speed: | 128 mph |
| Range: | 299 miles (sea level, no weapons, 10% reserve) |
| Ceiling: | 19,000 ft |
| Armament: | Air-to-air Stinger (ATAS) (2 round launcher); .50 caliber machine gun (500 rounds); HYDRA 70 (2.75 in) rockets (7-shot pod); HELLFIRE missiles (2-round launcher) |
|
|
|
| U.S. Army
Factfile found at: http://www.army.mil/fact_files_site/kiowa/index.html |
|
"Conduct armed reconnaissance, security, target acquisition and designation, command and control, light attack and defensive air combat missions in support of combat and contingency operations. Replaces AH-1 Cobra attack helicopters (those that function as scouts in air cavalry troops and light attack companies) and OH-58A and C Kiowas in air cavalry troops. Will be replaced by Comanche."With no Comanche in the works, the Pentagon is now fishing around for the light helicopter replacement. The shrinking military budget, produced by both conservative and liberal parties in office anxious to show responsibility to the home front, have created a helo force that frankly is decades behind the principal weapons of the Air Force and Navy they operate with. Not that we'd turn down a free Kiowa if we were handed a title today!

| Combat mission speed: | 167 mph |
| Combat range: | 300 miles |
| Combat endurance: | 2.5 hours |
| Length: | 49 ft 5 in |
| Mission weight: | 16,600 lbs |
| Armament: | HELLFIRE
missiles, 2.75" rockets and 30mm chain gun linked to the gunner's
helmet mounted sighting system |
| Crew: | 2 (pilot and co-pilot gunner) |
|
|
|
| U.S. Army Factfile found at: http://www.army.mil/fact_files_site/apache/index.html | |
| UH-60A |
UH-60L | |
| Mass gross weight: | 20,250 lbs | 22,000 lbs, 23,500 (external cargo) |
| Cruise speed: | 139 kt | 150 kt |
| Endurance: | 2.3 hrs | 2.1 hrs |
| Max range: | 320 nm | 306 nm |
| External load: | 8000 lbs | 9000 lbs |
| Internal load: | 2640 lbs (or 11 combat-equipped troops) | |
| Crew: | 4 (2 pilots; 2 crew chiefs) | |
| Armament: | Two 7.62mm machine guns | |
| |
||
| U.S. Army
Factfile found at:
http://www.army.mil/fact_files_site/blackhawk/ |
||
Chinook"Tier 1 aircraft may commonly be referred to as the UH-60L+. The UH-60L+ cockpit will incorporate Force XXI digital battlefield capability. All nav/com avionics and selected flight instruments will be replaced with Multifunctional Display (MFD). The first tier will provide life extension, digitization, and other enhancements to make the UH-60 relevant and effective on the modern battlefield.
Tier 2 aircraft may commonly be referred to as the UH-60(X) until formal designation is received. The second tier will focus primarily on performance related capabilities needed to support the Army Vision that can not be achieved today within acceptable cost, schedule and risk constraints. The achievement of tier 2 performance levels will rely on the development and qualification of technology that is currently not available. Current operator and maintainer UH-60A/L training material, devices, and simulators will be required to continue UH-60A/L training until the fully modernized UH-60(x) has replaced all systems in the field." 6
| Max gross weight: | 50.000 lbs |
| Empty weight: | 23,401 lbs |
| Max speed: | 170 knots / 184 mph |
| Normal cruise speed: | 130 knots / 137 mph |
| Rate of climb: | 1,522 ft/min |
| Rotor system: | three manual-folding blades per hub (two hubs); 225 revolutions per minute; 60-ft rotor span; |
| Troop capacity: | 36 (33 troops plus 3 crew members) |
| Litter capacity: | 24 |
| Sling-load capacity: | 26,000 lb center hook; 17,000 lb forward/aft hook; 25,000 lb tandem |
| Minimum crew: | 3 (pilot, co-pilot, and flight engineer) |
|
|
|
| U.S. Army
Factfile found at: http://www.army.mil/fact_files_site/chinook/index.html |
|
"CH-47D version, which remains the U.S. Army standard and features composite rotor blades, an improved electrical system, modularized hydraulics, triple cargo hooks, avionics and communication improvements, and more powerful engines that can handle a 19,500 lb load – nearly twice the Chinook’s original lift capacity. An upgrade program exists to remanufacture 300 of the current fleet of 425 CH-47D’s to the CH-47F standard. The MH-47E is the Special Forces variant of the Chinook and will be remanufactured to the MH-47G.
The Chinook’s cockpit accommodates two pilots and an observer. The communications suite includes jam resistant HF and UHF radio systems and the helicopter is equipped with an Identification Friend or Foe (IFF) interrogator. Three machine guns can be mounted on the helicopter, two in the crew door on the starboard side and one window-mounted on the port side. Additionally, the helicopter is equipped with a suite of countermeasure systems, which could include one or more of the following: a missile approach warner, jammers, radar warner, and chaff and flare dispensers.
The Chinook has a triple hook system, which provides stability to large external loads or the capacity for multiple external loads. Large external loads such as 155mm howitzers can be transported at speeds up to 260km/h using the triple hook load configuration. Multiple external loads can be delivered to two or three separate destinations in one sortie."

| Gross Weight: |
At IGE Hover 4,000 ft: 19,200 lbs; at service ceiling non-hover): 20,000+ lbs |
| Useful
Load: |
1,868 lbs (847 kg) |
| Speed: | 161 knots (140 KTAS) max, 130 mph (113 KTAS) cruise |
| Range: | >162 nm (> 300m) at 4000 ft. and 95 deg. F, loiter at 60 kots, 4000 ft, 4 hrs (Bell 407) |
| Length: | 36.7 (11.19m) (41.6ft X 7.7 ft. Rotor folded, 36.6ft X 24.1 ft. folded) |
| Width: |
Swath: 35.4 ft side-to-side.; Bell 407 Std: cabin and skids 8.8 ft (2.68m) Tail: 7.3 ft 2.2m) |
| Height: | 10.2 feet, 11 in. (3.32m), Swatch: 36.7ft (11.19m) front-to-back |
| Engine: | One Honeywell HTS900-2 turbine, 970 shp (723kW) |
| Rotor system: | Main: 35.4 ft diameter (10.67m), four blades, 7.8 ft ground clearance (2.36m) (Bell 407) Tail: |
| Sling-load capacity: | 26,000 lb center hook; 17,000 lb forward/aft hook; 25,000 lb tandem |
| Minimum crew: | 2 (pilot,
co-pilot) |
| Ceiling: |
20,000 ft. (1,219m) |
| Armament: | 0.50 cal Gatling gun, 7-tub 2.75" FFAR (foding fin rocket) launcher or 38 std rocket tube bundles |
| Other Features: |
|
|
|
|
| Bell ARH-70A Brochure (MILNET Mirror) (PDF: 2.6MB), Bell 407 Tech Specs (MILNET Mirror) (PDF: 953KB) |
|

| Max gross weight: | 7,903 lbs |
| Useful
Load: |
3,953
lbs |
| Max speed: | 145 knots |
| Length: | 33.4 ft |
| Width: |
5.7 ft |
| Height: | 11.5 ft |
| Rotor system: | 36.1 ft
main rotor with 6.4 ft. tail rotor |
| Troop capacity: | 8 |
| Litter capacity: | 24 |
| Sling-load capacity: | 26,000 lb center hook; 17,000 lb forward/aft hook; 25,000 lb tandem |
| Crew: | 3 (pilot, co-pilot, and flight engineer) |
| Ceiling (Max Hover) |
11,300 ft |
|
|
|
Of course, the chances of anyone in the DoD getting a chance to propose such programs is slim. The Navy and and Air Force still appear to be getting the lionshare of the defense budget. This is the usual DoD mistake, one which we have been accustomed to worrying about for over thirty years.
- Fast Track the scout program
- Investigate UAV/UCAV and remotely piloted versions to the full extent and if reasonable build a mix of operational capabilities using BOTH, not favoring one or the other.
- Take the Navy's approach to the next generation, the Helo X programs with 21st century goals not remake of 1960s/70s technology. Calling a UH-60 upgrade an X program is not funny and insulting to the American public's intelligence. This program should encompass the scout, transport, and attack chopper replacements with slow but well armored and deliver much more firepower with greater precision.
- Elect a Congress that is not anti-war/anti-weapons oriented. If we are going to have a military, then we have to continue to have the best. Short funding them is not only ludicrous, but dangerous. Quit whining about millions spent unwisely, weapons development will always require adjustments and occassionally will require better gear to follow. Overly criticial procurement policies stifle our ability to move forward AND push the technology.