Template:Infobox rocket engine/testcases
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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 |
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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
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| 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 |
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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
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| 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 |
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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
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| 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 | |
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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
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| Manufacturer | Yoyodyne |
|---|---|
| neutrino flux | |
| Proves once and for all whether neutrinos have mass. | |
| Performance | |
| Specific impulse | 0. or else ∞. Probably. |
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Zapp-o-tron Manufacturer Yoyodyne neutrino flux Proves once and for all whether neutrinos have mass. Performance Specific impulse 0. or else ∞. Probably.
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