H-53 Sea Stallion In Action by C. M. Reed, Ernesto Cumpian, Don Greer, Andrew Probert

By C. M. Reed, Ernesto Cumpian, Don Greer, Andrew Probert

H-53 Sea Stallion In motion КНИГИ ;ВОЕННАЯ ИСТОРИЯ H-53 Sea Stallion In motion (Aicraft quantity 174)ByChris ReedPublisher:Squadron/Signal courses Inc.2000 52PagesISBN: 0897474171PDF15 MBThe strongest helicopter in provider with the U.S. army, the Sikorsky H-53 has served with contrast with the Marine Corps. Air strength, and military in view that its first flight in 1964. each significant clash because Vietnam has obvious H-53s excited by a way. both bringing males and gear into difficulty spots, rescuing downed aircrews, evacuating civilians, or sweeping for mines. whereas older examples were retired, the more moderen CH-53E and MH-53K types, jointly w ith the lengthy serving and often-rebuilt Air strength PAVE LOWs. will proceed in ser­vice for future years. sharingmatrixletitbit zero

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1-6)] for R m = 104 km are given in Ref. 7. Calibration of the device is described also in Ref. 7. The minimum dust particle mass registered by FOTON made up 6X1O10 g. A group of particles is discussed below, which is determined by all three characteristics of their interaction with the screen: energy burst, impulse, and hole size. On V-l there were registered N0 = 275 of such particles. 2 X 10~4 cm2, was pierced by particles with m* = 5 X 10~9 g. Figure 3 shows the number of dust particles entering the screen of the device as a function of time (the summation was extended over a time interval of 30 s).

Because in the z//0 —> 0 limit, the distribution function is symmetric in cf,, only even k occur. Following the procedure adopted by St. Maurice and Schunk5 and Hubert 9 , we consider the moments of a particular order p = k+2£, and the convergence of the solution is considered vs the order p rather than in terms the number of basis functions M and N. III. Results and Discussion The ion distribution function was calculated vs the system variables, D1', i//fi and the mass ratio m/M with the recurrence relation for 14 B.

SW C H + ) ; km k mXs sin 3-105K: V-l R-4,5'10 km (exit) V" 3OO n* 17 km/s T« 4'1O4 sin' J K V-2 kmXs kmXs Fig. 1 continued. VEGA SPACECRAFT AERODYNAMICS Symbol V V R, 27 km v-2 1, 6'10' 5 1,35-1O55 , 2,63-io 5 entry 1,5'1O , e n t r y 1,4'10 5 , e n t r y Cometopause apex: GIOTTO PLASMAG 3, pp. 165-174 MAG MAG IMS RPA a, pp. 352-355 2, 2, 3, pp. 352-355 pp. 330-334 pp. 221 -225 2, pp. 349-352 C 4 + 5 ; > ' 1 O 4 km C GIOTTO) COLD COMETARY PLASMA BOUNDARY Symbol -< Y s R, km 1,5-10* PLASMAG 3, pp.

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