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The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight ... Cruise speed: 82 kn (94 mph, 152 km/h) at 10,000 ft (3,050 ...
Cruise speed: 105 kn (121 mph, 195 km/h) ... Cessna 150; Cessna 152; Grumman American AA-1; Liberty XL2; Piper PA-38 Tomahawk; Symphony SA-160; Whitney Boomerang ...
Design cruise, also known as the optimum cruise speed, is the most efficient speed in terms of distance, speed and fuel usage. [16] [17] [18] V cef: See V 1; generally used in documentation of military aircraft performance. Denotes "critical engine failure" speed as the speed during takeoff where the same distance would be required to either ...
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
Choosing any particular set of parameters will generate the needed power for a particular aircraft for those conditions. For instance a Cessna 150 at 2,500-foot (760 m) altitude and 90-mile-per-hour (140 km/h) speed needs about 60 horsepower (45 kW) to fly straight and level. The C150 is normally equipped with a 100-horsepower (75 kW) engine ...
At high-speed cruise, it can fly one pilot and four passengers over 1,150 nmi (2,130 km) in 2 h 49 min. It climbs to FL 410 in 24 min, 27% faster than its closest competitor, where it is 53 kn (98 km/h) faster than the Embraer Phenom 100 E. [ 8 ] With 150 produced since introduction in 2013, it became Cessna's entry-level jet after the Citation ...
2006 amateur built RV-9A. The architect of the line of Van's aircraft, Richard VanGrunsven, designed the RV-9 as a departure from the concepts of the earlier RV series.The earlier members of the RV series, starting with the single seat RV-3, were all designed to have light handling, aerobatic capabilities along with high cruise speeds and short takeoff and landing (STOL) capabilities.
This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
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