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The top horizontal line represents the maximum payload. It is limited structurally by maximum zero-fuel weight (MZFW) of the aircraft. Maximum payload is the difference between maximum zero-fuel weight and operational empty weight (OEW). Moving left-to-right along the line shows the constant maximum payload as the range increases.
With a 66 ft (20 m) wingspan, and a maximum payload of 3,800 lb (1,700 kg), the MQ-9 can be armed with a variety of weaponry, including Hellfire missiles and 500 lb (230 kg) laser-guided bomb units. [36] Its endurance is 30 hours when conducting ISR missions, which decreases to 23 hours if it is carrying a full weapons load. [37]
The C909CCF (COMAC converted freighter) is designed with a maximum payload of 9,467kg and is compatible with PMC, PAG and AKE cargo containers. [24] The first aircraft began conversion operations on 22 December, 2022 at GAMECO in Guangzhou, China. [ 41 ]
Family of 4×4 and 6×6 tactical trucks with 2.5-ton, 5-ton, 9-ton and 10-ton payload (U.S. tons) [1] Place of origin: United States: Service history; In service: 1996–present: Used by: United States Army and others (see Operators) Production history; Designer: Steyr of Austria (original); Stewart & Stevenson for FMTV requirement.
For those who needed yet more space, a Luton van body was offered, built on either the 255 or 350 chassis cabs, providing capacities of 11.3 m 3 (400 cu ft) (with 200 Series cab) or 15.6 m 3 (550 cu ft) (300 Series), and a maximum payload of almost two tonnes.
According to the manufacturer, these enable the Aksungur to cruise at a maximum speed of 180 km/h (110 mph) and carry a maximum payload of 750 kg (1,650 lb) [5] [6] to an altitude of 25,000 ft (7,600 m), or ascend to 35,000 ft (11,000 m) with a 150 kg (330 lb) payload. The aircraft's designed maximum payload is 375% greater than that of its ...
The UR-700M would have a payload capacity of 750 t (1,650,000 lb). [64] The only Universal Rocket to make it past the design phase was the UR-500 while the N1 was selected to be the Soviets' HLV for lunar and Martian missions. [65] The UR-900, proposed in 1969, would have had a payload capacity of 240 t (530,000 lb) to low earth orbit. It never ...
It is planned for a maximum payload capacity of 140,000 kg [31] to low Earth orbit (LEO), 50,000 kg to trans-lunar injection or 44,000 kg to Mars. [ 32 ] [ 33 ] Its first flight is expected by 2028 or 2029 in preparation for a lunar landing sometime in the 2030s; [ 34 ] a sample return mission from Mars has been proposed as first major mission ...