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  2. ACES II - Wikipedia

    en.wikipedia.org/wiki/ACES_II

    ACES is an acronym for Advanced Concept Ejection Seat. It is used in Fairchild Republic A-10 Thunderbolt II, McDonnell Douglas F-15 Eagle, General Dynamics F-16 Fighting Falcon, Lockheed Martin F-22 Raptor, Lockheed F-117 Nighthawk, Rockwell B-1 Lancer, WB-57, Northrop Grumman B-2 Spirit, and Mitsubishi F-2 aircraft. Over 10,000 ACES II seats ...

  3. Ejection seat - Wikipedia

    en.wikipedia.org/wiki/Ejection_seat

    This system is also used in the T-6 Texan II and F-35 Lightning II. The ACES II Ejection seat commonly used on United States Air Force jets. Through-Canopy Penetration is similar to Canopy Destruct, but a sharp spike on the top of the seat, known as the "shell tooth", strikes the underside of the canopy and shatters it. The A-10 Thunderbolt II ...

  4. Martin-Baker - Wikipedia

    en.wikipedia.org/wiki/Martin-Baker

    Martin-Baker claimed in 2022 that since the first live ejection test in 1945, [3] a total of 7,732 lives have been saved by the company's ejection seats. [4] Martin-Baker also manufactures what it calls "crashworthy" seats for helicopters and fixed-wing aircraft. As of 2012, over 20,000 crashworthy seats have been delivered.

  5. General Dynamics F-16 Fighting Falcon - Wikipedia

    en.wikipedia.org/wiki/General_Dynamics_F-16...

    [44] [91] The F-16's ACES II zero/zero ejection seat is reclined at an unusual tilt-back angle of 30°; most fighters have a tilted seat at 13–15°. The tilted seat can accommodate taller pilots and increases g -force tolerance; however, it has been associated with reports of neck aches, possibly caused by incorrect headrest usage. [ 92 ]

  6. Sheppard AFB pilot dies after ejection - AOL

    www.aol.com/sheppard-afb-pilot-dies-ejection...

    "An Air Force instructor pilot with the 80th Flying Training Wing died early this morning from injuries sustained when their T-6A Texan II ejection seat activated during ground operations here May 13.

  7. Lockheed Martin F-22 Raptor - Wikipedia

    en.wikipedia.org/wiki/Lockheed_Martin_F-22_Raptor

    The ejection seat was downgraded from a fresh design to the existing ACES II. Despite efforts by the contractor teams to rein in weight, the takeoff gross weight estimates grew from 50,000 to 60,000 lb (22,700 to 27,200 kg), resulting in engine thrust requirement increasing from 30,000 to 35,000 lbf (133 to 156 kN) class. [17]

  8. Multiple crew failures and wind shear led to January crash of ...

    www.aol.com/news/multiple-crew-failures-wind...

    A fiery January crash of a B-1 bomber in South Dakota was caused by multiple crew failures, terrible winter weather and a last-minute brush with wind shear that resulted in all four members ...

  9. Portal:Aviation/Anniversaries/July 13 - Wikipedia

    en.wikipedia.org/wiki/Portal:Aviation/...

    Capt. Darren S. Ruhnau, 27, of Niceville, Florida, assigned to the 60th Fighter Squadron, ejects safely. He and another F-15 had departed Eglin at 0835 hrs. for a training mission. "I'm just glad the ACES II ejection system worked as advertised", Ruhnau said in a statement, "and that the search-and-rescue guys were there to do the job."