Results 101 to 110 of about 94,203 (190)
Revista Mexicana de Fisica, 49, 191 (2003), 2012 Elementary concepts from general physics and thermodynamics have been used to analyze rocket propulsion. Making some reasonable assumptions, an expression for the exit velocity of the gases is found. From that expression one can conclude what are the desired properties for a rocket fuel.
arxiv
Five Solar Cycles of Solar Corona Investigations. [PDF]
Sol Phys, 2022 Antonucci E.
europepmc +1 more source
, 2019 In the modern era, the notion of space travel is generally one of greater acceptance and ease than in times previously. Moreover, a greater number of nations (and now even private entities) have the technological capabilities to launch manned and ...
Lashendock, Jack H.
core
UEG Week 2024 Moderated Posters
United European Gastroenterology Journal, Volume 12, Issue S8, Page 201-664, October 2024.
wiley +1 more source
The Ultimate Limits of the Relativistic Rocket Equation. The Planck Photon Rocket [PDF]
Acta Astronautica, Vol. 136, July 2017, Pages 144-147, 2018 In this paper we look at the ultimate limits of a photon propulsion rocket. The maximum velocity for a photon propulsion rocket is just below the speed of light and is a function of the reduced Compton wavelength of the heaviest subatomic particles in the rocket. We are basically combining the relativistic rocket equation with Haug's new insight on the
arxiv
The Early History of Heliospheric Science and the Spacecraft That Made It Possible. [PDF]
Space Sci Rev, 2022 Zank GP +10 more
europepmc +1 more source
Aerospace systems and mission analysis research - Solar electric space mission analysis Final report [PDF]
Mission analysis for solar electric propelled spacecraft on Mars Orbiter, Jupiter flyby, and asteroid belt exploration ...
Handelsman, M. +2 more
core +1 more source
UEG Week 2024 Poster Presentations
United European Gastroenterology Journal, Volume 12, Issue S8, Page 665-1360, October 2024.
wiley +1 more source
Lyapunov Orbits at L2 and Transversal Intersections of Invariant Manifolds in the Jupiter-Sun Planar Restricted Circular Three Body Problem [PDF]
arXiv, 2011 We present a computer assisted proof of existence of a family of Lyapunov orbits which stretches from L2 up to half the distance to the smaller primary in the Jupiter-Sun planar restricted circular three body problem. We then focus on a small family of Lyapunov orbits with energies close to comet Oterma and show that their associated invariant ...
arxiv
86th Annual Meeting of the Meteoritical Society (2024)
Meteoritics &Planetary Science, Volume 59, Issue S1, Page A1-A468, August 2024.
wiley +1 more source