TECHNICAL READOUT UD-4L 'CHEYENNE' UTILITY DROPSHIP

by Lee Brimmicombe-Wood and Dave Hughes transcribed by Livius Halupczok
The UD-4 'Cheyenne' is a versatile dropship and tactical transport employed in a primary role in the US Colonial Marines. Derived from an original Department of Defense requirement for a multi-role shuttle capable of lifting heavy payloads up to 16,000 kg, the UD-4 has become the definitive dropship design, influencing the shape of many derivatives and successors. The heart of the UD-4 is the power provided by the two General Dynamics TF- 900 Turbines, each producing 310 kN static thrust. This twin-engined configuration gives a degree of redundancy by still allowing the vessel to lift itself into orbit should one engine de damaged or shut down. Thrust can be vectored either through the side-bleed rotating nozzles to give VTOL capability, or through the stern nozzles for forward propulsion. The UD-4 utilises a lifting body configuration centered on its 324 cubic- metre payload bay. The bay is flanked by the two forward struts of the tricycle undercarriage and its floor comprises a hydraulic loading ramp that lowers directly to ground level. Froward of the loading bay is the spacious twin seat cockpit and to the stern is the tail assembly which houses the rear undercarriage strut, main fuel tanks and the contol surfaces. As far as is possible, the fuselage has integrated stealth characteristics including rounded leading surfaces, shielded compressor intakes, a butterfly tail and flash-coated cockpit transparencies. These features, in addition to the heavy use of rader and laser-absorbent composite materials throughout the airframe, serve to reduce the vessel's forward radar cross-section and thermal signature. The Cheyenne has a crew of two, comprising a Pilot and a Crew Chief/Weapons Officer. Control is fly-by-light with much of the pilot workload handled by the triple-redundant flight computer. This system is designed for maximum cockpit efficiency, registering all flight information on a bank of integrated CRT displays. The comprehensive Westinghouse avionics suite incorporates radar, optical, thermal and laser sensing arrays, and a communications data-link. Electronic counter-measures (ECMs) are provided internally by an ALQ-2004V multimode deception/barrage jammer, though this is supplemented by stern-mounted decoy dispensers firing chaff, flares and mini-jammers. The flight characteristics of the UD-4 prove it to be a stable and reliable vessel in the atmosphere-to-orbit interface and it is popular with its pilot. However, the airframe is only stressed to 6 g, and its air combat manoeuvrability is severly limited. If the UD-4 is forced into Air Combat Manoeuvring, a pilot's best option is to evade using the Cheyenne's vectored thrust capability or ECM. The 'L' variant tactical transport carries a wide array of powerful weaponry that can be used in dedicated support of its troop complement. Two main weapon bays fold out on extended pylons to deploy weapon hardpoints capable of carrying 16 x 150 mm unguided rockets each. Two secondary bays on the port and starboard side of the fuselage house a further 12 hardpoints for Air-to-Air/Air-to-Surface missles. The dropship also mounts a dedicated 20 kW Gatling Laser in a powered turret benath the nose. Target acquisition and weapons operation are handled by the Weapons Officer in the cockpit, although direct fire tasks utilising the Gatling Laser and Rockets can be carried out by the Pilot. In the Colonial Marines, the UD-4 is employed mainly as a tactical transport, having the capability to deploy troops and its own dedicated firepower direct from orbit to the operational area. Typical payloads into an operational Landing Zone (LZ) may include up to three fully equipped infantry squads or one M577 APC. The Cheyenne also has the capcity to carry up to 16,000 kg of stores. Typical mission profiles include Assault, Transport, CasEvac, Search and Rescue, Forward Supply, Close Air Support and Reconnaissance. The design of the UD-4 has proved highly successful and through refinement has prompted the production of several variants. These include the following: UD-4B - Original production variant powered by Avco Lycoming F23 Turbines producing 243 kN thrust each. Shorter by 1.5 metres that the later variants and with less payload space, this version was also equipped with the main weapons bays only. UD-4C - A gunship variant, this was the first to employ the secondary weapon bays and a dedicated gatling laser system. UD-4E - This was the UD-4B re-engined with F29-L-13 Turbines to gibe extended atmosheric range. UD-4H - The definitive production variant of this type, the UD-4H included a major redesign of many systems and components. The fuselage was stretched by 1.5 m to allow an extra 41 cubic metres of payload space and the engines were upgraded to TF-900 Turbines. The avionics fit was the first to include a broad-spectrum sensing arry and command data-link. Secondary missle bays and the Gatling Laser were now fitted as standard. UD-4J - A USCM life-extension program upgraded all existing UD-4B airframes to 'H' standard. This was designated the UD-4J. UD-4L - An upgrade of the 'H' version assault transport, the UD-4L incorporates an improved sensor and fire control system as well as being the first to include a multimode ECM/ECCM fit. Statistics for the UD-4L are as follows: Type: UD-4L Utility Dropship Crew: Pilot and Crew Chief/Weapons Officer Engines: Two General Dynamics TF-900 Turbines each rated at 310 kN dry thrust Dimensions: Lenth 24.3 m, Beam 18.2 m, Height 4.7 m Weights: Loaded 18,620 kg; Maximum Loaded 34,628 kg Performance: Maximum Acceleration (Loaded) 3.33 g; Maximum Acceleration (Fully Loaded) 1.79 g Armament: (Typical) 1 x 20 kW Gatling Laser; 32 x 150 mm unguided rockets; 6 x AGM-220 Air-To-Ground Missles; 4 x HiSARM Anti-Radiation Missles; 2 x AIM- 90 Short Range Air-To-Air Missles CMC - Colonial Marine Corps
Comments: For those who are familiar with military aircrafts, you will notice that the UD-4L is a future mix of the UH-1 and the AH-64 helicopter.

For any abbrevations look here.


Thanks to Livius Halupczok for this document.
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