The Yakovlev Yak-33 was a vertical takeoff and landing supersonic multi-purpose aircraft family, studied in the early 1960s, with variants of a basic design used to fulfill different roles, in a similar fashion to the Yak-25, Yak-27, Yak-28 family. Several configurations were studied including canard and tailless deltas, however matching supersonic performance with VTOL ability seriously compromised the design's ability to carry out its primary missions.
Specifications (Yak-33 estimated) Data from OKB Yakovlev: A History of the Design Bureau and its Aircraft,General characteristics Crew: 2 Length: 27 m (88 ft 7 in) Wingspan: 11 m (36 ft 1 in) Gross weight: 32,000 kg (70,548 lb) Max takeoff weight: 40,000 kg (88,185 lb) Powerplant: 2 × Kolesov RD-36-41 vectored thrust afterburning turbojets, 68.67 kN (15,440 lbf) thrust each dry, 156.96 kN (35,290 lbf) with afterburner Powerplant: 6 or 8 × lift engines turbojets, 29.43 kN (6,620 lbf) thrust each Performance
Maximum speed: Mach 3 Cruise speed: M2M2 Range: 4,000 km (2,500 mi, 2,200 nmi) Armament
Bombs: Tactical nuclear weapons or conventional bombs
References
Further reading Gordon, Yefim; Gunston, Bill (1997). Yakovlev aircraft since 1924 (1st ed.). London: Putnam. ISBN 0851778720.
