Jump to content

Antonov An-50: Difference between revisions

From Wikipedia, the free encyclopedia
Content deleted Content added
RussBot (talk | contribs)
m Robot: Editing intentional link to disambiguation page in hatnote per WP:INTDABLINK (explanation)
Adding/improving reference(s) WP:FEB24
Line 19: Line 19:
|}
|}


The '''Antonov An-50''' was a planned [[Soviet Union|Soviet]] airliner with four turbojets. It was planned by [[Antonov]] in the first part of the 1970s. The aircraft was never built.
The '''Antonov An-50''' was a planned [[Soviet Union|Soviet]] airliner with four turbojets. It was planned by [[Antonov]] in the first part of the 1970s. The aircraft was never built.<ref>{{Cite web |title=Antonov-50 |url=https://www.globalsecurity.org/military/world/russia/an-50.htm |access-date=2024-02-03 |website=www.globalsecurity.org}}</ref>


Antonov made the plans based on the [[Antonov An-24|An-24R]], but it would have had four turbojets with 14.7&nbsp;kN [[thrust]] each, instead of the two turbojets used earlier. The turbojets were planned to be built together with the undercarriage, under the inner wings. There were no other major changes planned. The plans were complete in 1972, however no aircraft were built.
Antonov made the plans based on the [[Antonov An-24|An-24R]], but it would have had four turbojets with 14.7&nbsp;kN [[thrust]] each, instead of the two turbojets used earlier. The turbojets were planned to be built together with the undercarriage, under the inner wings. There were no other major changes planned. The plans were complete in 1972, however no aircraft were built.

Revision as of 00:09, 3 February 2024

An-50
An–50 plastic model
Role Airliner
National origin Soviet Union
Manufacturer Antonov
Status Cancelled
Number built Not built
Developed from Antonov An-24

The Antonov An-50 was a planned Soviet airliner with four turbojets. It was planned by Antonov in the first part of the 1970s. The aircraft was never built.[1]

Antonov made the plans based on the An-24R, but it would have had four turbojets with 14.7 kN thrust each, instead of the two turbojets used earlier. The turbojets were planned to be built together with the undercarriage, under the inner wings. There were no other major changes planned. The plans were complete in 1972, however no aircraft were built.

It was planned to weigh 24600 kg gross, and it would have had a 490 km/h speed at 9400 m altitude.

External links

  1. ^ "Antonov-50". www.globalsecurity.org. Retrieved 2024-02-03.