Category talk:Rocket engines of the United Kingdom

Missing rocket engines

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Here's a list from Skomer "United Kingdom Aerospace and Weapons Projects: Rocket Engines". Skomer.

This could form a basis for an expansion project.

Name	Maker	Date	Type	Fuel	Description	Origin	Rating	Remarks	Use
Armstrong Siddeley Alpha	Armstrong Siddeley		Liquid	HTP (High Test Peroxide) / Kerosene.		Armstrong Siddeley's first rocket.			Intended for RATO
Armstrong Siddeley Delta	Armstrong Siddeley			HTP / kerosene		Family of research engines developed by RPR and Armstrong Siddeley.			Intended for a ballistic missile. Superseded by Rolls-Royce RZ2.
E.237	Napier		Turborocket			Submission to the NGTE specification TE 10/56
FPS.146	Rolls-Royce_Limited		turbo-rocket.						Future Project Study. Proposed for the HSA APD 1019/E6 as an alternative to the BS.1012 combination engines on APD 1019/E2. Cancelled.
KP.1			liquid	HTP / kerosene					Early rocket engine for guided weapons. Used on RTV.2
KP.3			liquid	HTP / kerosene	Regeneratively liquid-cooled combustion chamber.				Early rocket engine for guided weapons. Used on GPV
KP.4			liquid	HTP / kerosene	Ceramic lined combustion chamber.				Early rocket engine for guided weapons. Used on GPV.
Lizzie			liquid	Liquid Oxygen (LOX) and petrol	First liquid fuelled engine in UK.	Rocket engine developed by RPE. Used in LOP/GAP with Liquid Oxygen and petrol. RTV1 fuelled with Liquid Oxygen and methanol/water.	Rated at 2000lbf (8.9kN).
NK.1			liquid	Red Fuming Nitric Acid (RFNA) (oxidizer) and kerosene					Sea Slug. Replaced by Foxhound
NRE.11	Napier		Liquid						rocket engine for guided weapons.
NRE.17	Napier		liquid	HTP / kerosene	Uncooled chamber and nozzle.		Rated at 2,000lbf (8.9kN).		rocket for missile applications.
NRE.19	Napier		monopropellant	HTP / catalyst					Helicopter rotor tip applications Tested on a Saro Skeeter
P170	Armstrong Siddeley		Turborocket study.			Submission to the NGTE specification TE 10/56
PP.27	Rolls-Royce_Limited		Turborocket study.			Submission to the NGTE specification TE 10/56. PP.27 may have been the Brochure title.
PR.23	Bristol Siddeley		liquid	HTP / kerosene	Very small, vernier manoeuvring engine.		Rated at 500lbf (0.3kN).
PR.27	Armstrong Siddeley				four chamber rocket engine.				Proposed for the Bristol Siddeley Small Satellite Launcher.
PR.37	Armstrong Siddeley				small boost rocket.		Rated at 170lbf (0.7kN).		Intended for GAF Jindivik
PR.38	Armstrong Siddeley				small four chamber rocket engine.		Rated at 2 - 3000lbf (8.9 - 13.3kN).		Proposed for Black Prince (Rocket) 3rd stage. Cancelled.
RB9/2	Armstrong Siddeley					Early designation for Blue Steel engine. Possibly led to Stentor.
RB545	Rolls-Royce_Limited				Liquid Air Cycle engine for HOTOL	Designed to power a single stage to orbit vehicle.			HOTOL single stage to orbit (SSTO) vehicle
Rolls-Royce RZ12	Rolls-Royce_Limited		liquid	LOX / kerosene	Twin installation of Rolls-Royce RZ2 for Blue Streak
RZ20	Rolls-Royce_Limited		liquid	LOX / LH2					engine for ELDO Europa rocket. Cancelled, 2 examples built
Spartan	Bristol Siddeley		liquid		Storable liquid propellant with hypergolic combustion.				For RATO.
TRR/37	Napier								Two to be fitted in underwing pods on the Hawker P.1105 Hunter F.Mk6
Cuckoo (Rocket motor)			solid
Jackdaw (Rocket motor)			solid			Development tests of Blue Steel "Avro Blue Steel stand-off missile".