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Fouga CM.175 Zéphyr

Military Aircraft

The Fouga CM.175 Zéphyr was a French two-seat carrier-capable jet trainer of the 1950s, developed for the French Navy from the land-based Fouga CM.170 Magister. The prototype, first designated CM-170M Esquif, flew on 31 July 1956 and was soon redesignated the CM.175 Zéphyr, and carrier trials followed from HMS Eagle and HMS Bulwark off the French coast in 1957 and 1958. Compared with the Magister it had an arrester hook, a modified structure and a strengthened undercarriage, a nose-mounted light, and sliding canopy hoods that could be locked open during carrier launches and landings because it had no ejection seats. It was powered by two Turbomeca Marboré IIA turbojets. One rocket pod could be carried under each wing for weapons training. Thirty-two aircraft were delivered, the first production aircraft flew on 30 May 1959, and the type entered service in October 1959 with the deck landing school at Hyères. It was retired in 1994.

Facts
Year
1956 1
Engine Class
Jet 1
Status
Retired from service 1
Top Speed (km/h)
715 1
Mass (kg)
2150 1
Maximum Mass (kg)
3200 1
Engine
Two Turbomeca Marboré IIA turbojets 1
Comparison
Body Style
Aircraft (no road body style) 1
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Source Fouga CM.175 Zéphyr (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
a 1950s French two-seat carrier-capable jet trainer
Sources
1. Fouga CM.175 Zéphyr (Wikipedia)
  • Design and development, first flight
    the prototype first flew on 31 July 1956
  • Lead
    was a 1950s French two-seat carrier-capable jet trainer
  • Specifications, powerplant
    Powerplant: 2 × Turbomeca Marboré IIA turbojets, 3.92 kN (882 lbf) thrust each
  • Specifications, empty weight
    Empty weight: 2,150 kg (4,740 lb)
  • Specifications, max takeoff weight
    Max takeoff weight: 3,200 kg (7,055 lb)
  • Specifications, maximum speed
    Maximum speed: 715 km/h (444 mph, 386 kn)
  • Lead, retirement
    The Zéphyr was retired in 1994
  • Lead, country of origin
    a 1950s French two-seat carrier-capable jet trainer
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