I think in the payload.
The load it can carry after fuel.
Max payload that can be carried on an aircraft can be derived as following; Max Payload = MTOW - (OEW + Fuel Capacity). In case of B727-200, MTWO = 95,208 kg, OEW = 45,360 kg and max fuel capacity = 37,020 L (29,616 kg). Hence Max Payload on B727-200 is; Max Payload = MTOW - (OEW + Fuel Capacity); or Max Payload = 95,208 - (45,360 + 29,616) or Max Payload = 95,208 - 74,976 kgs hence Max Payload = 20,052 kgs Hope this helps. Cheers - Arun Kumar Singh (AKS)
Max payload that can be carried on an aircraft can be derived as following; Max Payload = MTOW - (OEW + Fuel Capacity). In case of B727-200, MTWO = 95,208 kg, OEW = 45,360 kg and max fuel capacity = 37,020 L (29,616 kg). Hence Max Payload on B727-200 is; Max Payload = MTOW - (OEW + Fuel Capacity); or Max Payload = 95,208 - (45,360 + 29,616) or Max Payload = 95,208 - 74,976 kgs hence Max Payload = 20,052 kgs Hope this helps. Cheers - Arun Kumar Singh (AKS)
The greater the mass of the payload, the more fuel (and more money) it requires to get it into orbit.
There are several other words or synonyms listed for payload. These words include charge, haul, freight, goods, load, and weight.
Depends on the Fuel amount and payload. Max range is 2,069 Miles.
The required runway length depends on the payload and, the fuel on board the aircraft. If your looking at relatively full payload and, maximum weight on board you can see some 747's using full length runway departures which can be over 12,000 feet. So there really is not a required runway length till you get specific with payload and, fuel on board.
There are no perfect rhymes for the word payload.
You only have a few choices: -- reduce the total weight (mass) of the rocket and its payload -- burn fuel faster -- burn fuel at the same rate but use fuel with a greater specific impulse
If your reading this than your a true idiot because the bay is used to carry the extra fuel. Will Thompson
DOW (Dry Operating Weight) in aviation refers to the weight of an aircraft when it is empty and without any fuel or payload. It includes the weight of the structure, systems, equipment, and furnishings of the aircraft. DOW is used to calculate the aircraft's performance, fuel calculations, and maximum payload capacity.