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Microcosm 356N
Microcosm LOx/Kerosene rocket engine. First stages. Hardware. Funded under AFRL SBIR Phase 1 contract of 2006. Ablative chamber, LOX/Jet A propellant engines designed for very low-cost, robust design margins.

Status: Hardware. Date: 2000-2004. Thrust: 356.00 kN (80,031 lbf).

In 2006 Microcosm began development of a new 356,000-newton engine under an AFRL SBIR Phase 1 contract. Both the 20,000-pound-force and 80,000 pound-force engines were follow-on developments to the successful 5,000-pound-force engines. All were ablative chamber, LOX/Jet A propellant engines designed for very low-cost, robust design margins, moderate chamber pressures, high reliability, and expendable applications.

Propellant Formulation: Lox/Jet A.



Country: USA. Propellants: Lox/Kerosene. Agency: Microcosm.

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