「lbf.」の共起表現一覧(2語右で並び替え)
該当件数 : 37件
Ratio 11:25, 7,260 | lbf (68130-68142 and 68152-68153) |
ypical bolt cutter yields 20 kilonewtons (4,500 | lbf) of cutting force for a 250 newtons (56 lbf) fo |
stiffness is typically measured in pound force ( | lbf) per inch. |
Low gear 11,435 | lbf (50.87 kN) |
High gear 7,965 | lbf (35.43 kN) |
The Terrier first stage produced 58,000 | lbf (258 kN) thrust, while the ASROC second stage p |
Maximum power at T-O is 4,850 | lbf (21.58 kN) with a specific fuel consumption of |
-force (7.6 kN) of thrust was increased to 1920 | lbf (8.5 kN) and later to 2800 lbf (12.5 kN) for th |
d rocket strapon boosters-each providing 53,000 | lbf (236 kN) thrust-to the standard Thor core stage |
5C small high-bypass turbofan engine with 3,190 | lbf (14.2 kN) thrust. |
urbojets were substituted, producing only 4,900 | lbf (21.8 kN) of thrust with afterburner rather tha |
were used for a total tractive effort of 6,200 | lbf (28 kN) and a maximum speed of 10 mph (16 km/h) |
ment Landing System, J35-A-29 engine with 5,560 | lbf (24.7 kN) of thrust, and the ability to carry a |
estinghouse turbojets, raising power from 1,600 | lbf (7 kN) to 3,000 lbf (13 kN) each; since the lar |
tt & Whitney Canada PW-305 turbofans with 5,200 | lbf (23 kN) thrust each, first flight 16 June 1990, |
ul Armstrong Siddeley Sapphire engines of 7,200 | lbf (32 kN) of thrust instead of Rolls-Royce Avons, |
e Apollo Service Module, with a thrust of 6,000 | lbf (27 kN) and a Specific impulse of 313 seconds, |
Ratio 19:19, Low gear 12,600 | lbf (56 kN), High gear 4,705 lbf (20.93 kN) (68154- |
he E-1, which provided about 360,000 to 380,000 | lbf (1,700 kN), four of which would reach the requi |
ements exceeded the max engine thrust of 21,000 | lbf (93 kN). |
iameter, nominal tractive effort rose to 31,170 | lbf (138.7 kN). |
, to get the tractive effort up to above 40,000 | lbf (a major goalpost), the cylinders were enlarged |
This variant produces about 16,500 | lbf (73,000 N) of thrust.. |
RCS thrusters: sixteen x 100 | lbf (440 N) in four quads |
rcraft features the GE CF34-8C5 engines, 13,360 | lbf (59,400 N) thrust with APR, and added leading e |
This created 150 | lbf (700 N) of thrust and lifted the vehicle 12 fee |
The "T2" variant is uprated to 18,070 | lbf (80,400 N) of thrust and is used on the Tu-334- |
Variant of the engine with 11,760 | lbf (52,300 N) of thrust proposed for use in the Su |
gines, as originally designed, delivered 39,700 | lbf (177,000 N) tractive effort, with 16-inch bore |
35 short stories and one novel (Dreaming Creek, | LBF Books, Oct. 2008). |
Morpheus's 4000 | lbf engine permitted NASA to design a larger vehicl |
manding and would be limited to about 1 million | lbf in the short term anyway. |
boost including 320 | lbf residual thrust from the turbine at 2,050 rpm ( |
each capable of generating 3.9 kilonewtons (880 | lbf) of thrust, for orbital manoeuvres. |
eased the tractive effort from 24,300 to 27,340 | lbf (108 to 121.6 kN). |
ng 102 hp of mechanical power and 105 ft (32 m) | lbf of torque using Bosch M1.3 fuel injection. |
rs, a liftoff thrust of 365 kilonewtons (82,100 | lbf), a total mass of 3,385 kilograms (7,463 lb), a |
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