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Neutron is a partially reusable medium-lift two-stage launch vehicle under development by Rocket Lab.Announced on 1 March 2021, the vehicle is designed to be capable of delivering a payload of 13,000 kg (28,700 lb) to low Earth orbit in a partially reusable configuration, [3] and will focus on the growing megaconstellation satellite delivery market. [4]
Data from Poser - PWS - Podlaska Wytwórnia Samolotów: PWS-50, Polish Aircraft 1893–1939 General characteristics Crew: 2 Length: 8.02 m (26 ft 4 in) Wingspan: 10.97 m (36 ft 0 in) Height: 2.92 m (9 ft 7 in) Wing area: 29.2 m 2 (314 sq ft) Empty weight: 900 kg (1,984 lb) Gross weight: 1,250 kg (2,756 lb) Fuel capacity: 150 L (40 US gal; 33 imp gal) Powerplant: 1 × PZL- Wright J-5B Whirlwind ...
The XUV700 is offered with one petrol engine and one diesel engine option. The former is a 2.0-litre four-cylinder turbocharged mStallion unit which is tuned to produce 200 PS (197 hp; 147 kW) and 380 N⋅m (38.7 kg⋅m; 280 lb⋅ft).
It displaces 6,614 lb (3,000 kg) and carries 2,667 lb (1,210 kg) of ballast. [ 1 ] [ 2 ] The boat has a draft of 5.09 ft (1.55 m) with the standard keel and is fitted with a Faryman a40 diesel engine of 8 to 12 hp (6 to 9 kW) with hydraulic (Hydromarine) transmission for docking and manoeuvring.
Oil pressure on the clutch plates was, after the facelift, regulated by a centrifugal valve integrated in the electric axial six piston oil pump. Compared to the previous generation, the Haldex 5 system was 1.4 kg lighter (ca. 6.6 kg without oil) and simpler as it didn't contain an oil pressure accumulator.
The S-IVB had a dry mass of about 23,000 pounds (10,000 kg) and, when fully fueled, weighed about 262,000 pounds (119,000 kg). [ 64 ] The S-IVB was the only rocket stage of the Saturn V small enough to be transported by the cargo plane Aero Spacelines Pregnant Guppy .
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The following table takes values as an example for the specific fuel consumption of several types of engines. For specific engines values can and often do differ from the table values shown below. Energy efficiency is based on a lower heating value of 42.7 MJ/kg (84.3 g/(kW⋅h)) for diesel fuel and jet fuel , 43.9 MJ/kg (82 g/(kW⋅h)) for ...