Article image
Article image
Article image
Article image

THIS NEW HELICOPTER, developed by the Lockheed-California Company, is the first rotary-wing aircraft to use successfully the stable gyroscopic effects inherent in a rigid rotor. The gyroscopic force is the key to the machine’s outstanding flight stability and manoeuvrability. A distinguishing feature is the gyroscopic ring beneath the rotor. The aircraft weighs 2000lb and is powered by a 140h.p. engine. It has a three-bladed, 32ft-diameter main rotor, and a conventional tail rotor.

This article text was automatically generated and may include errors. View the full page to see article in its original form.
Permanent link to this item

https://paperspast.natlib.govt.nz/newspapers/CHP19620213.2.48

Bibliographic details

Press, Volume CI, Issue 29746, 13 February 1962, Page 7

Word Count
72

THIS NEW HELICOPTER, developed by the Lockheed-California Company, is the first rotary-wing aircraft to use successfully the stable gyroscopic effects inherent in a rigid rotor. The gyroscopic force is the key to the machine’s outstanding flight stability and manoeuvrability. A distinguishing feature is the gyroscopic ring beneath the rotor. The aircraft weighs 2000lb and is powered by a 140h.p. engine. It has a three-bladed, 32ft-diameter main rotor, and a conventional tail rotor. Press, Volume CI, Issue 29746, 13 February 1962, Page 7

THIS NEW HELICOPTER, developed by the Lockheed-California Company, is the first rotary-wing aircraft to use successfully the stable gyroscopic effects inherent in a rigid rotor. The gyroscopic force is the key to the machine’s outstanding flight stability and manoeuvrability. A distinguishing feature is the gyroscopic ring beneath the rotor. The aircraft weighs 2000lb and is powered by a 140h.p. engine. It has a three-bladed, 32ft-diameter main rotor, and a conventional tail rotor. Press, Volume CI, Issue 29746, 13 February 1962, Page 7