Examples
{{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 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
}}
{{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
}}
{{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
}}
{{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;;
}}