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A German tractor pulling team designed a vehicle, named "Dragon Fire", around a methanol-fueled version of this engine; [1] this modified [2] engine is said to weigh 3,200 kg (7,100 lb) including the gearbox, for use in the 4.5 ton tractor pulling class, making 8,000 hp (6,000 kW) at 2,500 rpm.
Bullet mass/type Velocity Energy; 480 gr (31 g) RN/FMJ: 2,378 ft/s (725 m/s) 6,288 ft⋅lbf (8,525 J) 500 gr (32 g) Solid: 2,500 ft/s (760 m/s)
The J-2, commonly known as Rocketdyne J-2, was a liquid-fuel cryogenic rocket engine used on NASA's Saturn IB and Saturn V launch vehicles. Built in the United States by Rocketdyne, the J-2 burned cryogenic liquid hydrogen (LH 2) and liquid oxygen (LOX) propellants, with each engine producing 1,033.1 kN (232,250 lb f) of thrust in vacuum.
50 kg: Bye Tsukimi Namiki W 5–0 Ruhafzo Haqnazarova W 5–0 Nikhat Zareen W 3–2 Wu Yu L 0–5 Jutamas Jitpong: 54 kg — Chang Yuan L 2–3 Did not advance Porntip Buapa: 57 kg Chandrakala Thapa W 5–0 Lin Yu-ting L 0–5 Did not advance Thananya Somnuek: 60 kg Bibinashastamo Kholova W RSC