Template:Infobox rocket engine/testcases

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Examples

Sprite
Country of originBritain
Manufacturerde Havilland
ApplicationRATO
hydrogen peroxide monopropellant
Performance
Thrust5,000 lbf (22.2kN)
Total impulse55,000 lbf seconds
Burn time16 seconds
Propellant capacity39 gallons
{{infobox rocket engine
  |name=Sprite
  |country_of_origin=Britain
  |manufacturer=[[de Havilland]] 	
  |purpose=[[RATO]]

  |type=mono
  |fuel=[[hydrogen peroxide]] 
  |capacity=39 gallons

  |thrust=5,000 lbf (22.2kN)
  |burn_time=16 seconds
  |total_impulse=55,000 lbf seconds
}}

BS.605
Country of originBritain
ManufacturerBristol Siddeley
ApplicationRATO, swing-out from fuselage
Liquid-fuel engine
Propellanthydrogen peroxide / kerosene
Performance
Thrust4,000 lbf
Burn time30 seconds
Dimensions
Length1067 mm
Diameter305 mm
Dry weight166 kg
{{infobox rocket engine
  |name=BS.605
  |country_of_origin=Britain
  |manufacturer=[[Bristol Siddeley]] 	
  |purpose=[[RATO]], swing-out from fuselage

  |type=liquid
  |oxidiser=hydrogen peroxide
  |fuel=kerosene

  |thrust=4,000 lbf 
  |burn_time=30 seconds

  |length=1067 mm
  |diameter=305 mm
  |dry_weight = 166 kg
}}

Gamma 301
Country of originBritain
ManufacturerBristol Siddeley
Application1st stage booster
PredecessorGamma 201
SuccessorGamma 8
Liquid-fuel engine
PropellantHydrogen peroxide / kerosene
Mixture ratio8:1 (approx.)
Configuration
Chamber4, gimballed in opposed pairs
Performance
Specific impulse250
Burn time120 seconds
{{infobox rocket engine
  |name=Gamma 301
  |type=liquid
  |country_of_origin =Britain

  |designer=
  |manufacturer= [[Bristol Siddeley]]

  |predecessor=[[Gamma 201]]
  |successor=[[Gamma 8]]

  |purpose = 1st stage booster
  |oxidizer=Hydrogen peroxide
  |fuel=kerosene

  |mixture_ratio= 8:1 (approx.)

  |combustion_chamber= 4, gimballed in opposed pairs

  |thrust_at_launch= 19,000 - 21,000 (lbf) 

  |specific_impulse= 250
  |burn_time = 120 seconds
}}

Waxwing
Country of originBritain
DesignerBristol Aerojet
ManufacturerPERME
ApplicationApogee kick motor
Solid-fuel motor
Corestar
Casingspherical
Used in
Black Arrow, 3rd stage


{{infobox rocket engine
  |name=Waxwing

  |country_of_origin =Britain
  |designer=[[Bristol Aerojet]]
  |manufacturer=[[PERME]]

  |purpose=Apogee kick motor

  |type=solid
  |casing=spherical
  |core=star

  |used_in= [[Black Arrow]], 3rd stage
}}

Zapp-o-tron
ManufacturerYoyodyne
neutrino flux
Proves once and for all whether neutrinos have mass.
Performance
Specific impulse0. or else ∞. Probably.
{{infobox rocket engine
  |name=Zapp-o-tron
  |type=neutrino flux
  |description=Proves once and for all whether [[neutrino]]s have mass.
  |specific_impulse=0. or else ∞. Probably.

  |manufacturer=[[Yoyodyne]]

  |style=border: thin groove blue; background-color: #ffc;;
}}