SNECMA M45

The SNECMA M45, also called the SNECMA Mars, was a turbojet engine designed and produced by SNECMA in France during the late 1950s and early 1960s. The M45 was the precursor to a family of turbojet and turbofan engines, culminating in the collaborative Rolls-Royce/SNECMA M45H, high bypass turbofan engine.

Variants

Data from: Aircraft Engines of the World 1964/65
;M45A: A compact moderate thrust turbojet.
;M45A-3:for civil applications.
;M45AF:Aft-fan turbofan engine intended for civil aircraft.
;M45B:Turbojet with afterburning for military aircraft.
;M45B-3:With afterburner.
;M45F-3:Civil non-afterburning for small airliners / business jets.
;M45L-1:Lightweight civil version for small business jets.
;SNECMA/Bristol Siddeley M45G:Afterburning turbofan engine for AFVG, from the civil M45F.