Air Commando Fighters of World War II by Edward Young

By Edward Young

Air Commando combatants of worldwide struggle II

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Linder commented that the person solving this problem does not know if ‘‘thrust’’ refers to the thrust required for takeoff, or the thrust for the nominal cruising speed, or indeed to the maximum engine thrust. It is up to the engineer, or perhaps his manager, to further refine the problem. For our BotE estimate, detailed below, we assume that the quantity of interest is ‘‘takeoff thrust’’, which as propulsion engineers know is close to the maximum thrust that a jet engine generates. The objective of Linder’s thesis was a survey of MIT mechanical engineering Sec.

2, I’ve drawn a sketch of a crude 747 aircraft with some relevant dimensions. These dimensions are based on my personal visual recollection of the 747 jet aircraft that I flew on as a passenger to Australia about 10 years ago. 3 Gathering the input data needed for the calculation I recall the 747 had four engines and some pretty large wings. I estimate that the wing, on each side of the fuselage, is close to 100 feet in length, or about 30 m. The width of each wing is perhaps approximately 1/3rd of its length, call it 10 m.

Configuration of the overall Hubble Space Telescope system [14, p. 14]. Sec. 5 Estimating the size of the optical system for the Hubble Space Telescope 29 System requirements for the HST Our primary estimation goals are to calculate the basic optical telescope scales and the optical performance necessary for this unique space telescope to meet the following major resolution and sensitivity system requirements: . High angular resolution—the ability to image fine detail. High sensitivity—the ability to detect very faint objects.

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