What is the minimum takeoff speed, Mass and Force applied for a typical Jet
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What is the minimum takeoff speed, Mass and Force applied for a typical Jet

[From: ] [author: ] [Date: 11-12-20] [Hit: ]
for example,Maximum Takeoff Weight 875,000 lb (396,Maximum Range 7,260 nautical miles (13,Maximum Fuel Capacity 57,......
If there are any professionals what is the name of the jet, minimum-take off speed and total Mass of the Jet in question? And also what is the Force applied to it?

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They are all different, pick one and look it up online.

Boeing 747-400, for example, (there are a lot of different versions of the 747)
From the reference
Maximum Takeoff Weight 875,000 lb (396,890 kg)
Maximum Range 7,260 nautical miles (13,450 km)
Maximum Fuel Capacity 57,285 U.S. gal (216,840 L)
Typical Cruise Speed 0.85 Mach
at 35,000 feet 567 mph (913 km/h)
They don't spec takeoff speed, that is calculated on a flight-by-flight basis and based on payload, amount of fuel, and (important) altitude of airport.

other (unverified reference) has: Take off speed for 747-400 fully loaded is 155-160 knots or almost 300 km/h or 180 mph.

wikipedia
In 1989, a Qantas 747-400 flew non-stop from London to Sydney, a distance of 9,720 nmi (11,190 mi, 18,001 km), in 20 hours and 9 minutes to set a commercial aircraft world distance record. This was a delivery flight with no commercial passengers or freight aboard. During testing, the first 747-400 built also set a world record for the heaviest airliner takeoff on June 27, 1988, on a flight to simulate heavy-weight stalls. The flight had a takeoff weight of 892,450 pounds (404,810 kg), and in order to satisfy Fédération Aéronautique Internationale regulations, the aircraft climbed to a height of 6,562 feet (2,000 m).
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