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171

3 2. General spacecraft description. The IUE spacecraft is shown in mission orbit configuration and in an exploded view in figures 2-1 and 2-2 respectively.

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Source URL: ines.ts.astro.it

Language: English - Date: 2001-02-23 07:05:19
    172Spaceflight / Rocketry / Spacecraft propulsion / Rocket propulsion / Transport / Astrodynamics / Single-stage-to-orbit / Solid-fuel rocket / Propellant / Tsiolkovsky rocket equation / Saturn V / Specific impulse

    IAF–98–V.3.07 A FLEXIBLE REUSABLE SPACE TRANSPORTATION SYSTEM S. S. Pietrobon Small World Communications

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    Source URL: www.sworld.com.au

    Language: English - Date: 2007-11-30 00:13:44
    173

    Effects of spin-orbit coupling on the BCS-BEC crossover Luca Salasnich Dipartimento di Fisica e Astronomia “Galileo Galilei”, Universit` a di Padova, Italy

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    Source URL: materia.fisica.unipd.it

    Language: English - Date: 2013-01-23 10:15:32
      174Physics / Quantum mechanics / Atomic physics / Electromagnetism / Magnetism / Rotational symmetry / Hyperfine structure / Spinorbit interaction / Dynamic nuclear polarisation / Coulomb blockade / Spin

      RAPID COMMUNICATIONS PHYSICAL REVIEW B 81, 201305共R兲 共2010兲 Disentangling the effects of spin-orbit and hyperfine interactions on spin blockade S. Nadj-Perge,1 S. M. Frolov,1 J. W. W. van Tilburg,1 J. Danon,1,2

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      Source URL: kouwenhovenlab.tudelft.nl

      Language: English - Date: 2012-01-11 09:42:03
      175

      1 1. Introduction. The IUE spacecraft was launched in January 1978 from Cape Canaveral, Florida. It was the first astronomical satellite to have been placed into a geosynchronous orbit; and, also, the first scientific s

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      Source URL: ines.oat.ts.astro.it

      Language: English - Date: 2001-02-23 07:05:19
        176

        All planets move in ellipses. A planet that moves in a perfectly circular orbit is actually an ellipse with its eccentricity (e) = 0, a parabola has e = 1 and a hyperbola the e > 1. So the closer to zero the planets ecce

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        Source URL: www.bambi.net

        Language: English - Date: 2005-07-30 23:44:58
          177

          ORBIT. IUE was successfully launched on January 26, 1978 at 17:36 UT on a Delta launch vehicle. The spacecraft was introduced into geosynchronous orbit through one stage of spin-stabilized flight and two stages of

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          Source URL: ines.ts.astro.it

          Language: English - Date: 2001-02-23 07:05:19
            178

            Computing the Orbit of a Comet 156 This historic image of the nucleus of Halley’s Comet by the spacecraft Giotto in

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            Source URL: spacemath.gsfc.nasa.gov

            Language: English - Date: 2010-05-06 13:08:56
              179

              Chapter 12 Gravitation What makes things fall down? What keeps the moon in orbit around the earth? What keeps the earth in orbit around the sun?

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              Source URL: ionaphysics.org

              Language: English - Date: 2016-01-24 13:06:35
                180

                1 Celestial Mechanics A Miscellaneous Problems 1. A comet, whose mass m is negligible compared with that of the Sun, is moving around the Sun in a parabolic orbit. When at an end of its latus rectum it collides with and

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                Source URL: astrowww.phys.uvic.ca

                Language: English - Date: 2015-02-09 14:43:35
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