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Napier Scorpion

Space and Rocket Propulsion

The Napier Scorpion was a family of British liquid-fuelled rocket engines developed and made at the Napier Flight Development Establishment at Luton in the late 1950s, designed as boosters to improve take-off and high-altitude performance. Its regeneratively cooled chamber burned kerosene with high-test hydrogen peroxide, and a single steam-driven turbo-pump fed both propellants. The single-chamber Scorpion first ran on 19 May 1956 and flew in the bomb-bay of an English Electric Canberra a day later. A Canberra fitted with the twin-chamber Double Scorpion exceeded 70,000 feet on 28 August 1957, a world altitude record. The programme was cancelled in February 1959.

Facts
Classification
Fuel or Cycle
Rocket Propellant 1
Year
1956 1
Connections

Of Make

Source Napier Scorpion (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Napier Scorpion (Wikipedia)Lead, maker
Quote, Lead, maker
developed and manufactured by Napier
Sources
1. Napier Scorpion (Wikipedia)
  • Design and development, propellants
    High-Test Peroxide (HTP) as oxidiser and Kerosene as fuel
  • Design and development, first run
    First run on 19 May 1956, the N.Sc.1 Scorpion was also fired in the air on the following day
  • Lead, maker
    developed and manufactured by Napier
  • In Group: Rocket Engines, Lead, kind of engine
    The Napier Scorpion series of rocket engines are a family of British liquid-fuelled engines
  • Part Of: English Electric Canberra, Design and development, first flight
    mounted in the bomb-bay of an English Electric Canberra B.2
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