Armstrong Siddeley Screamer

{{short description|1950s British aircraft rocket engine}}

{{Use dmy dates|date=February 2018}}

{{Use British English|date=February 2018}}

{{Infobox aircraft begin

|name = Screamer

|image = File:AS Screamer RRHT.jpg

|caption = Screamer engine on display at the Rolls-Royce Heritage Trust, Derby

}}{{Infobox aircraft engine

|type=Rocket engine

|manufacturer=Armstrong Siddeley

|national origin=United Kingdom

|first run=19 May 1954

|major applications=

|number built =

|program cost =

|unit cost =

|developed from =

|variants with their own articles =

|developed into =

}}

The Armstrong Siddeley Screamer was a British rocket engine intended to power the Avro 720 manned interceptor aircraft (Avro's competitor to the Saunders-Roe SR.53 for a rocket-powered interceptor). Thrust was variable, up to a maximum of {{convert|8000|lbf|kN|abbr=on}}.{{cite journal

|journal=Flight

|title=Armstrong Siddeley Screamer

|url=http://www.flightglobal.com/pdfarchive/view/1956/1956%20-%201014.html

|archive-url=https://web.archive.org/web/20121023094116/http://www.flightglobal.com/pdfarchive/view/1956/1956%20-%201014.html

|archive-date=23 October 2012

|url-status=dead

|type = PDF

|date=27 July 1956

|pages=160–164

}}{{cite journal

|title=Rockets for Aircraft Propulsion

|first=S., RAeS

|last=Allen

|journal=The Aeroplane

|date=7 Dec 1951

}}{{cite journal

|journal=Flight

|title=ROCKET-MOTOR DESIGN: A Paper by the Chief Engineer of Armstrong Siddeley Motors (Rocket Division)

|first=S., RAeS

|last=Allen

|url=http://www.flightglobal.com/pdfarchive/view/1956/1956%20-%201483.html?search=screamer

|archive-url=https://web.archive.org/web/20160306160515/https://www.flightglobal.com/pdfarchive/view/1956/1956%20-%201483.html?search=screamer

|archive-date=6 March 2016

|url-status=dead

|type = PDF

|date=19 October 1956

|accessdate=27 November 2014

|pages=637–638

}}

Design and development

Work on the Screamer started in 1946, with the first static test at Armstrong Siddeley's rocket plant at Ansty in March 1954.{{cite journal

|journal=Flight

|title=Scorpion and Screamer

|url=http://www.flightglobal.com/pdfarchive/view/1956/1956%20-%200930.html

|archive-url=https://web.archive.org/web/20180504091602/https://www.flightglobal.com/pdfarchive/view/1956/1956%20-%200930.html

|archive-date=4 May 2018

|url-status=dead

|format = PDF

|date=13 July 1956

|pages=76

|ref=Flight, 13 July 1956, Scorpion and Screamer

}} The programme was cancelled, as was the Avro 720, before flight testing.{{cite book

|title=A Vertical Empire: The History of the UK Rocket and Space Programme, 1950-1971

|author=C.N. Hill

|year=2001

|publisher=Imperial College Press

|isbn=1-86094-268-7

|page=28

|url=https://books.google.com/books?id=AzoCJfTmRDsC&dq=Armstrong+Siddeley+Screamer&pg=PA28

}}

In 1951, a Gloster Meteor F.8 was experimentally fitted with a Screamer mounted below the fuselage.{{cite web

|author=Keith Meggs

|title=A Man and his Machines

|url=http://www.ctie.monash.edu.au/hargrave/MEGGS_meteor.html

|access-date=18 April 2008

|archive-date=29 March 2008

|archive-url=https://web.archive.org/web/20080329140348/http://www.ctie.monash.edu.au/hargrave/MEGGS_meteor.html

|url-status=dead

}}

The Screamer project was cancelled in March 1956, at a reported total cost of £650,000.{{cite journal

|journal=Flight

|title=Cancelled projects: the list up-dated

|url=http://www.flightglobal.com/pdfarchive/view/1967/1967%20-%201672.html

|archive-url=https://web.archive.org/web/20180612162641/https://www.flightglobal.com/pdfarchive/view/1967/1967%20-%201672.html

|archive-date=12 June 2018

|url-status=dead

|format = PDF

|date=17 August 1967

|pages=262

|ref=Flight, Flight, 17 August 1967, Cancelled projects list

}}

Engines on display

Specifications

{{rocketspecs

|ref=

|type=Variable thrust liquid-propellant rocket engine

|length= 78.5 in (199.4 cm)

|diameter= 27 in (68.6)

|weight= 470 lb (213.2 kg)

|fueltype=Kerosene

|oxidiser= Liquid oxygen (LOX) and filtered water (coolant)

|capacity=

|pumps=Three pumps

|thrust=9,500 lb (42 kN) at 40,000 ft (12,200 metres) (estimated)

|thrust/weight=

|burn time=

|fuelcon=

|specfuelcon=

}}

See also

{{aircontent

|see also=

|related=

|lists=

|similar engines=

}}

References

{{reflist}}