Propellant
The present invention relates to a propellant in liquid or gel form, in particular for rocket engines, comprising: -an inorganic salt as the oxidising agent, wherein the inorganic salt has an oxygen content of at least 60 weight %; and -a solvent as the fuel, comprising a monovalent or divalent alco...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | The present invention relates to a propellant in liquid or gel form, in particular for rocket engines, comprising: -an inorganic salt as the oxidising agent, wherein the inorganic salt has an oxygen content of at least 60 weight %; and -a solvent as the fuel, comprising a monovalent or divalent alcohol, a nitroalkane and/or an ionic liquid in which nitrate is the anion, wherein the solvent has an oxygen content of from 30 to 55 weight %, wherein the inorganic salt is dissolved in the solvent. |
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