HH-71 CSAR-X Team Successfully Demonstrates Aerial Refueling Flights

PR Newswire - 2/21


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The Lockheed Martin and AgustaWestland HH-71 Team successfully conducted aerial refueling tests between an RAF AW101 Merlin Mk3 helicopter and an Italian Air Force KC-130J tanker, further demonstrating the aircraft’s superior capabilities and low-risk approach for the U.S. Air Force’s Combat Search and Rescue (CSAR-X) requirement.

refuel2.jpgThe successful fuel transfer occurred over the south of England on February 13, marking the first time a British helicopter demonstrated air-to- air refueling capability. The AW101 and RAF test pilots successfully plugged the helicopter’s refueling probe to each of the tanker’s two wing station drogues on the first attempt. The sorties were flown at 4,000 ft altitude, with both aircraft traveling at 127 knots. All trial objectives were completed with multiple in-flight refueling events successfully achieved up to the maximum Merlin Mk3 flying weight of 34,400 lbs.

refuel3.jpg“To support our win strategy of providing the U.S. Air Force the lowest risk offer, we completed the aerial refueling tests prior to contract award,” said Dan Spoor, Lockheed Martin’s CSAR-X vice president. “With this proven aerial refueling capability, the aircraft has demonstrated all critical capabilities required for the CSAR mission. The aircraft exceeds the technical readiness level required by the CSAR-X RFP.”

All Merlin Mk3 helicopters have air refueling capability and this trial is the latest step in providing an Operational Release for in-service Merlin Mk3 helicopters fitted with the advanced design BERP III and BERP IV rotor blades.

“The robust NDI air refueling technology employed on the HH-71 combined with its excellent cockpit visibility, significant probe to blade clearance, precise handling qualities and high power margins result in the most capable, low risk aerial refueling helicopter for the CSAR-X mission,” said Stephen C. Moss, chief executive officer of AgustaWestland North America. “The fact that the fuel transfer occurred on the first attempt and that the sorties were flown with both the BERP III and the BERP IV advanced rotor systems, makes the successful trials all the more significant.”

The tests were performed through the collaboration of the HH-71 Team, Britain’s Ministry of Defence, the Italian Air Force, and the NATO Maintenance and Supply Agency.

UP CLOSE WITH THE HH-71
Production-standard BERP IV advanced main rotor blades
  • BERP IV productionized in 2007
  • Minimize brownout (21,500 successful combat desert landings using the BERP rotor blade)
  • Reduce internal noise and vibration effects on crew and passengers
  • Produce 15% better downwash velocity than required by the RFP
  • Quiet, less detectable by the enemy; delays enemy load/preparation timeline for guns/MANPADs/RPGs
  • Comfort — low vibration and low noise increase warfighter preparedness and situational awareness
  • Improve hover performance
  • Reduce cruise fuel consumption
Large, Unobstructed Door
  • Cabin access designed by Flight Engineers (FE), Aerial gunners (AG) and Pararescuemen (PJ)
  • Supports rapid, safe IP and PJ hoists
  • Stokes litter remains horizontal
  • No external obstructions (sponsons, probes, steps, etc.)
  • Work upright in cabin and unobstructed by guns, ammo, radios, walls
Smaller and Clearer LZ
  • Brownout is the #1 cause of helicopter accidents in combat. The HH-71 effectively eliminates brownout
  • Advanced, production-standard BERP IV blades push dust, sand and snow away from landing area
  • Never lose visual contact with ground during approach to landing
  • Faster, safer landings with or without coupled landing
  • Smaller footprint improves survivability, with more landing options and less hover time for faster, safer rescues
360-Degree Overlapping Threat Suppression
  • Right gun-mount and hoist design allow for simultaneous hoist and gunnery, with superior field of fire
  • 360° coverage and 200° overlapping coverage
  • Able to fire aft gun while simultaneously conducting AIEs (fast rope, rappel) from the ramp
Triple Redundant Engines
  • Adds 15 knots of top-end speed
  • Allows sustained cruise in combat or adverse weather even if one engine disabled (OEI)
  • Significantly reduces the size of the avoid zone during low-speed, low-altitude maneuvers
  • Can fly Two Engines Operating (TEO) to conserve fuel and extend range/endurance during ferry flight segments