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Antares e.V.

20 kN Testbed

Lander

100 kN Testbed

Hybrid Launcher
- Details
- Feasibility (back to Hybrid Launcher)

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Feasibility

Before we haven't finished our 20 kN testbed and developed a working small hybrid rocket engine at least in the 1kN class, we won't go any further.

Let's suppose we allready would have developed our engine and it worked well, what would be our next steps?

  1. We could use our engine as heart of a scientific aerial vehicle to develop an avionic system for lift-off and even landing applications. We call this shortly the 'Lander'.
  2. We could reuse our experience in designing, building and testing a small hybrid engine for the development of a much bigger rocket engine. Let's say an engine in the 100kN class.
  3. We should merge these two former steps to a commercial application. A small hybrid rocket launcher that can compete with comparable launching systems on the world market is our goal.