By Peter M. Grosz
LFG Roland D.II КНИГИ ;ВОЕННАЯ ИСТОРИЯ LFG Roland D.II (Windsock Datafile 47)By Peter M. GroszPublisher: Albatros Productions Ltd199440 Pages ISBN: 0948414626PDF17 MBhe LFG Roland D.II used to be a German single-seat fighter of global conflict I. the sort was once synthetic by means of Luftfahrzeug Gesellschaft, and likewise by means of Pfalz Flugzeugwerke below license.The D.II used a plywood monocoque fuselage. layers of plywood strips have been spirally wrapped in opposing instructions over a mould to shape one 1/2 a fuselage shell. The fuselage halves have been then glued jointly, coated with a layer of material, and doped. the higher wing used to be connected to the fuselage through a wide important pylon, tremendously impairing the pilot's ahead imaginative and prescient. Armament consisted of dual "Spandau" LMG 08/15 computer weapons buried within the fuselage decking.The D.II was once at the start powered via a a hundred and sixty hp Mercedes D.III engine, giving a most sensible pace of 105mph at sea point. Later plane, precise D.IIa, have been powered by means of an a hundred and eighty hp Argus As.III. The As.III provided bad functionality above 3,000 m and the D.IIa used to be normally relegated to operations at the jap Front.Nicknamed Haifisch (shark) for its smooth visual appeal, the D.II and D.IIa proved commonly unpopular in provider because of negative fields of view and heavy controls. besides the fact that, it's also mentioned that the airplane had fairly delicate controls, quite within the yawing plane. the sort is understood to were been utilized by Jasta 25 at their Canatlarzi base in Macedonia in 1917. importing BitroadDepositfiles eighty five
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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.