Template:Infobox rocket engine/examples

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[edit] Examples

Sprite
Country of Origin Britain
Manufacturer de Havilland
Application RATO
hydrogen peroxide monopropellant
Performance
Thrust 5,000 lbf (22.2kN)
Total impulse 55,000 lbf seconds
Burn time 16 seconds
Propellant capacity 39 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 Origin Britain
Manufacturer Bristol Siddeley
Application RATO, swing-out from fuselage
Liquid-fuelled engine
Propellant hydrogen peroxide / kerosene
Performance
Thrust 4,000 lbf
Burn time 30 seconds
Dimensions
length 1067 mm
Diameter 305 mm
Dry weight 166 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 Origin Britain
Manufacturer Bristol Siddeley
Application 1st stage booster
Predecessor Gamma 201
Successor Gamma 8
Liquid-fuelled engine
Propellant Hydrogen peroxide / kerosene
Mixture ratio 8:1 (approx.)
Configuration
Chamber 4, gimballed in opposed pairs
Performance
Specific Impulse 250
Burn time 120 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 Origin Britain
Designed by Bristol Aerojet
Manufacturer PERME
Application Apogee kick motor
Solid motor
Core star
Casing spherical
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
Manufacturer Yoyodyne
neutrino flux
Proves once and for all whether neutrinos have mass.
Performance
Specific Impulse 0. 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;;
}}