Roket hibrida

Roket hibrida adalah roket dengan motor roket yang menggunakan propelan di dua bagian yang berbeda dari materi - satu padat dan yang lain baik gas atau cairan. Konsep roket hibrida dapat ditelusuri kembali setidaknya 75 tahun.
Hybrid roket memiliki keunggulan dibandingkan kedua roket cair dan roket padat terutama dalam hal kesederhanaan, keamanan, dan biaya.
Referensi
Wikimedia Commons memiliki media mengenai Hybrid rocket engines.
- Developing and testing of a 2kN hybrid rocket engine (Jerman)
- Hybrid Rocket Engines, AspireSpace, membership-based organisation (in UK) Diarsipkan 2018-07-22 di Wayback Machine. (particularly see technical papers Diarsipkan 2018-07-22 di Wayback Machine.)
- Portland State Aerospace Society paraffin hybrid links
- Hybridrocket, Private page (Jerman)
- WARR, students developing hybrid engines Diarsipkan 2011-12-06 di Wayback Machine. (Jerman)
- Hit09 S.r.l Company - Advanced Solution for Aerospace Application
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