Metodebevisregistrering
Hohmann Transfer
The Hohmann transfer is a maneuver that transfers a spacecraft between two circular orbits using two impulsive burns (velocity changes). Introduced by German engineer Walter Hohmann in 1925, it is the most fuel-efficient method for coplanar orbital transfers when the transfer time is not severely constrained. The transfer orbit is an ellipse tangent to both the initial and final orbits.
Kilderegistrering
Citater kopieret ordret fra metodens kilderegistrering. Ingen påstandsniveauverifikation er udledt heraf.
Hohmann Transfer Orbit
Taksonomisk metoderegistrering · process-pipeline / applied-physics
- Hohmann, W. (1925). Die Erreichbarkeit der Himmelskörper. R. Oldenbourg. · URL
- Curtis, H. D. (2013). Orbital Mechanics for Engineering Students (3rd ed.). Butterworth-Heinemann. · ISBN 978-0-08-102133-0
- Vallado, D. A., Crawford, P., Hujsak, R., & Kelso, T. S. (2006). Revisiting Spacetrack Report #3: Orbit Determination using Modern Computers. In AIAA/AAS Astrodynamics Specialist Conference. · DOI 10.2514/6.2006-6753
Kuraterede påstande
Påstande gemt i bevis-loggen, hver med sin egen vurdering.
Ingen kuraterede påstande endnu
Denne visning opfinder ikke en påstandsvurdering, når loggen ingen har.
Relaterede metoder
Genereret fra metodegrafen og vist som maskinelt foreslåede relationer — ingen bevispåstand er udledt.