| Signature mark | NL 230/2424 GF |
|---|---|
| Subject | Diagramm (1) |
| Title | Interrelation between energy yield, propellant fraction of weight at take-off, as well as characteristic cruising speed attainable, for adiabatic rocket systems, and for diabatic, photonic, rocket systems |
| Contains | Kurvendiagramm mit eingezeichneten Formeln und Berechnungsgrundlagen zu den Möglichkeiten irdischer, langsamer interplanetarer, schneller interplanetarer und interstellarer Raumfahrt |
| Note | Titel vereinfacht (ohne Formelzeichen); Lichtpause für die englischsprachige Fassung der Arbeit Eugen Sängers "Atom-Raumfahrzeuge: Atomraketen für Raumfahrt" (vgl. NL 230/2427); deutschsprachige Fassung des Diagramms siehe NL 230/2425 GF |
| Date | ca. 1959 - 1960 |
| Scope | 1 Bl. hs. |
| Formal information |
Format (HxB):
32 x 44 cm Languages: Englisch |
| Rights notice | CC BY-SA 4.0 |
| Permalink | https://digital-dev.deutsches-museum.de/item/NL-230-2424-GF |
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