«APOSELENIUM»に関連するポーランド語の本
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1
The Moon in the Post-Apollo Era - Strona 37
... at 23 h 21 min UT; the mid-course manoeuvre was executed 44 hr later; and injection into a circumlunar orbit (or distance from the surface varying between 196 km and 1871 km from periselenium to aposelenium) occurred on November 1, ...
2
Concise encyclopedia of astronautics - Strona 117
It moves in an orbit whose peri- selenium is 350 km from the lunar surface and whose aposelenium is 1017 km up. The orbit is inclined at 71° 54' to the lunar equator and the satellite's period of revolution is 2 h 58 min 15 sec. On 28 August ...
3
The Moon in the Post-Apollo Era - Strona 37
... at 23 h 21 min UT; the mid-course manoeuvre was executed 44 hr later; and injection into a circumlunar orbit (or distance from the surface varying between 196 km and 1871 km from periselenium to aposelenium) occurred on November 1, ...
4
Proceedings of the International Lunar Conference ... - Strona 162
The capture begins in - 116 days, when E=0, Vh=V„=0 (point C). ln ~ 14 days after that, the spacecraft goes to the final periselenium F, distances in periselenium r, =1,838 km, in aposelenium ra » 75, 000 km. The flight from point D to point F is ...
Steve M. Durst, American Astronautical Society, 2004
On February 19, a mid-course maneuver was executed as a result of which the station was transferred to an elliptical orbit having an aposelenium of 100 km and a periselenium of 21 km. To ensure the station's landing at the pre-determined ...
Center for Foreign Technology, 1972
6
Astronomical Contributions
executed 44 hours later; and injection into a circumlunar orbit (of distance from the surface varying between 196 km and 1871 km from periselenium to aposelenium) occurred on November 1, 20h 27m U.T., 92.5 hours after launch. After 23 ...
University of Manchester, 1968
7
Periodic, Quasi-Periodic and Chaotic Motions in Celestial ... - Strona 375
Note that to reduce the periselenium altitude from 598 km to the nominal altitude (200km), one needs only 5m/s. Using a traditional strategy the same coverage properties can be obtained by varying, for example, the inclination at aposelenium ...
Alessandra Celletti, Sylvio Ferraz-Mello, 2007
TABLE 13.2 Kinematic characteristics of the artificial lunar satellites (1966–68) Altitude (in km)b Injection into Number of Total number - in a tian a • • Spacecraft Period Inclination (Periselenium) (Aposelenium) lunar orbit End of mission days in ...
9
Celestial Mechanics: The Waltz of the Planets - Strona 7
For Earth- orbiting bodies it is perigee and apogee; for the Moon, periselenium and aposelenium; and so on (the generic form is 'apocentre' and 'pericentre'). The term 'Keplerian motion' also has a wider meaning, and is not restricted to ...
Alessandra Celletti, Ettore Perozzi, 2007
10
Fundamental Spacecraft Dynamics and Control - Strona 26
Öx XXXXXIXDA) 22%22% 22.22% Čx) 222 222 2222 ÇXXX 88.8×888. & $88.8888.888.882 & 8. : * Ó © © : : # 3. © © Č% 8 8 8% 8 %2 Figure 2.6 Canonical units perihelion, aphelion; periselenium, aposelenium respectively. Let 2c = distance ...
