The OH-58D Kiowa Warrior is a two-place single engine armed reconnaissance helicopter. The OH-58D's highly accurate navigation system permits precise target location that can be handed-off to other engagement systems. The OH-58D has an infrared thermal imaging capability and can display night vision goggle flight reference symbology. It's laser designator/laser rangefinder can provide autonomous designation for laser-guided precision weapons. Air-to-Air Stinger (ATAS) issiles provide the Kiowa Warrior with protection against threat aircraft.The primary mission of the Kiowa Warrior is armed reconnaissance in air cavalry troops and light attack companies. In addition, the Kiowa Warrior may be called upon to participate in the following missions or tasks:
The Mast Mounted Sight (MMS) is one of the key elements of the Kiowa Warrior. Its unique day/night capabilities allow the crew to scan the battlefield with the ability to acquire, identify, and derive the coordinate locations of potential targets.The US Navy selected the Kiowa Warrior Mast Mounted Sight for use on their ships. They were so pleased with it's performance that they entered into a program to update the technology in the existing platform. Their current Mast Mounted Sight II sight is smaller, lighter in weight, and half the cost of the US Army MMS. In addition, the optics have been upgraded through the application of technology insertion. The dollar cost avoidance in acquisition, operations and support cost, and spare components to support this system on the Kiowa Warrior is potentially significant. The AIM-1 MLR (and DLR), a class IIIb infrared (IR) laser, provides a beam of light invisible to the naked eye. Its beam is said to be effective for aiming at ranges up to 3km. It is designed to operate in conjunction with standard night vision devices (its beam's impact point visible). The AIM-1 laser is boresighted to a point 2.8 inches vertically above the .50 Cal machine gun barrel bore center line of sight at a distance of 500 inches. This provides the proper offset for firing at a range of 1000 meters.
The principal difference between the Kiowa Warrior and its immediate OH-58D predecessor is a universal weapons pylon on both sides of the aircraft capable of accepting combinations of the semi-active laser Hellfire missile, the Air-to-Air Stinger (ATAS) missile, 2.75" Folding Fin Aerial Rocket (FFAR) pods, and a 0.50 caliber machine gun. In addition to these weapons, the Kiowa Warrior upgrade includes changes designed to provide improvements in air-to-air and air-to-ground communications, mission planning and management, available power, survivability, night flying, and reductions in crew workload through the use of on-board automation and cockpit integration.
Since the last OA conducted in FY94, the Army determined that modifications in mission and equipment over time have created a deficiency in the Kiowa Warrior autorotation capability. In general terms, the cumulative addition of new equipment caused the weight of the aircraft to increase dramatically, meaning that in the event of an engine failure or other similar occurrence, the aircraft lost some of its original autorotative capability, causing the aircraft to descend faster and experience an extended ground slide upon touchdown. As a result, the Army developed a two-phase Safety Enhancement Program (SEP) to reduce the safety risk to Kiowa Warrior aviators. The SEP consists of both training and material changes.An improved version of the T-703 (R-3) engine will be installed which provides higher reliability and double the current overhaul interval, greater hot day power, and a Full Authority Digital Electronic Control (FADEC). The FADEC provides automatic rotor speed control, inflight restart, and performance recording, as well as more precise fuel metering capabilities. Additionally, an integrated body and head restraint system, a cockpit air bag system, and energy absorbing seats will be installed to enhance survivability in any crash situation. Beginning in March 1997, a number of improvements were introduced into new production OH-58Ds resulting from Task Force XXI exercises that took place at Fort Irwin, CA in March 1997, to demonstrate the Army's concept of the "digital battlefield". These improvements include an improved Allison 250-C30R/3 650 shp engine equipped with an upgraded hot section to improve high-altitude/hot-day performance. The C30R/3 will be fitted with a full authority digital electronic control system that will replace the hydromechanical fuel control unit. The improved production Kiowa Warrior will have an integrated cockpit control and display system, master control processor with digital map and video crosslink, along with an improved data modem, secure radio communications, and a GPS embedded in the inertial navigation system. Additional improvements include an infrared jammer, infrared suppressor, radar warning receivers, and a laser warning detector to improve aircraft survivability. The robust sensor capabilities of the KW in its mission as an armed reconnaissance aircraft, would be greatly enhanced by more effective communications within todayís digitized battlefield. By using the highly integrated avionics already on the aircraft, this capability can be added with only minor hardware and software changes. Video Image Crosslink (VIXL) provides the KW with the capability to send and receive still frame images over one of the FM radios. The VIXL consists of a circuit card installed in the IMCPU. In 1996 the KW Product Managerís Office (PMO) developed four VIXL ground stations, which consist of an Aviation Mission Planning Station (AMPS) with a Tactical Communication Interface Modules (TCIM) and a SINCGARS radio. The ground stations will be used to transfer VIXL images on the ground. Improved Mast Mounted Sight System Processor (IMSP) will replace the current configuration MMS System Processor (MSP). The product improved aircraft will include a new high-speed digital signal processor that will provide improved tracking capabilities by split-screen in both TV and Thermal Imaging Sight (TIS) modes, low contrast target tracking, simultaneous multi-target tracking of up to six targets, moving target indicator, aided target recognition, and automatic reaquiring of targets lost due to obstruction. The operator video display will reflect real time TV zoom and still frame capabilities. The IMSP enhancements consist of the use of high-speed Gallium Arsenide based digital signal processor integrated circuits in the MMS signal processor. The Circuit Card Assembly count in the processor will be reduced from 30 to 16. This reduction and use of state-of-the-art component technology enhances reliability, maintainability, and supportability. The IMSP will provide for enhanced growth and will not require substantial aircraft hardware changes. An update to the aircraft software, however, is required to execute the enhanced functions of the upgraded processor. This provides for future insertion of neural net automatic target recognition, identification of friend or foe, passive ranging, and real-time image enhancements. Form and fit of the existing MMS system processor is maintained, and is backwards compatible with the MMS System Processor (MSP). As of July 1997, all aircraft delivered from the Bell Helicopter production lots will have the IMSP installed. All retrofit aircraft will be equipped MSPs. As the MSPs are removed through attrition, they are replaced with IMSPs.
The addition of weapons, improved cockpit integration, and better navigational capability have resulted in an aircraft that is much more capable than its predecessor. Furthermore, the potential enhancements to mission planning and management provided by the aviation mission planning system (AMPS) and data transfer system (DTS) were very apparent during the DSUFTP. All of these improvements were achieved without any noticeable impact on readiness, as indicated by the aircraft's operational availability.
|Height||12 feet 10.6 inches|
|Length||41 feet 2.4 inches|
|Rotor diameter||35 feet|
|Maximum gross weight||4,500 pounds (unarmed);|
5,500 pounds (armed)
|Maximum airspeed||125 KIAS|
|Cruise airspeed||80 KIAS|
|Cargo hook capacity||2,000 pounds|
|Litter capacity||4 (externally)|
|Troop-carrying capacity||6 (externally).|
|Aircraft survivability equipment||