Template:Infobox rocket engine/testcases

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-fuel engine
Propellant	hydrogen peroxide / kerosene
Performance
Thrust	4,000 lbf
Burn time	30 seconds
Dimensions
Length	1067 mm
Diameter	305 mm
Dry mass	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-fuel 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
Designer	Bristol Aerojet
Manufacturer	PERME
Application	Apogee kick motor
Solid-fuel 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;;
}}