VJ 101

The EWR VJ 101 was an experimental West German jet fighter vertical takeoff/landing (VTOL) tiltjet aircraft. VJ stood for Versuchsjäger, (German for "Experimental Fighter"). The 101 was one of the first V/STOL designs to have the potential for eventual Mach 2 flight. During the 1950s, as various nations took an interest in developing VTOL-capable aircraft, the German Federal Government issued a request to the nation's recently revived aviation industries for them to study possible designs for such aircraft. In response, in 1960, German engine manufacturer MAN Turbo commenced work on a suitable engine in close cooperation with British engine manufacturer Rolls-Royce Limited. Likewise, aircraft firms Heinkel, Bölkow and Messerschmitt performed their own studies before coming together to form a joint venture company, EWR, for the purpose of developing and manufacturing their design for a supersonic VTOL fighter aircraft, which was soon designated as the VJ 101 D. The Federal Ministry of Defence (BMVg) were suitably impressed to place an order for a pair of experimental prototypes to be produced to demonstrate the design's capabilities. A pair of prototype aircraft, collectively known as the VJ 101 C and individually known as the X-1 and X-2, were constructed and participated in a five-year test program. The intention was for the VJ 101 to eventually be developed as the basis for a successor for the Luftwaffe's inventory of American Lockheed F-104G Starfighter interceptors. However, development of the VJ 101 C was greatly complicated by the changing requirements of the BMVg, who decided to transform the aircraft's envisioned mission profile from the interceptor role to a more general fighter instead, greatly changing the performance requirements for it to fulfil. During 1968, development of the VJ 101 was ultimately cancelled.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Entwicklungsring Süd
- First flight
- 1963-04-10
Specifications
- Cruise speed
- 140 kt
- Max speed
- 1.1 kt
- Max takeoff weight
- 13,228 lb
- Powerplant
- Rolls-Royce/MAN Turbo RB.145
- Engines
- 6
- Seats
- 1
- Length
- 51.5 ft
- Wingspan
- 21 ft
- Height
- 13.5 ft
- Number built
- 2
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.