Hypergolic two-component system for space propulsion and use of a hypergolic two-component system

DE202025004200U1Undetermined Publication Date: 2026-07-09DEUTSCHES ZENTRUM FÜR LUFT UND RAUMFAHRT E V
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Patent Information

Application Number
DE202025004200
Authority / Receiving Office
DE · DE
Patent Type
Utility models
Current Assignee / Owner
Filing Date
2025-12-18
Publication Date
2026-07-09
Estimated Expiration
2035-12-31
Patent Text Reader

Abstract

Hypergolic two-component system for space propulsion, comprising an oxidizer and a fuel which are provided separately and are brought into contact with each other in a thruster to react, wherein the oxidizer comprises hydrogen peroxide, characterized in that the fuel is a multi-component mixture comprising ammonium thiocyanate, a molecular liquid and an ionic liquid comprising a thiocyanate anion and one or more cations.
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Citation Information

Patent Citations

  • Hypergolic two-fuel system for rocket engines

    DE102019119598A1

  • Hypergolic dual-fuel system for hybrid rocket engines

    DE102021118007A1