Template:Infobox rocket engine/testcases
| This is the template test cases page for the sandbox of Template:Infobox rocket engine. to update the examples. If there are many examples of a complicated template, later ones may break due to limits in MediaWiki; see the HTML comment "NewPP limit report" in the rendered page. You can also use Special:ExpandTemplates to examine the results of template uses. You can test how this page looks in the different skins and parsers with these links: |
Examples
| 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
}}
| 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
}}
| 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
}}
| 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
}}
| 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;;
}}
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