Bloodhound SSC Vehicle Technical Specification: configuration 11, June 2012
Rolls-Royce EJ200 Specification
Item | Unit | Condition | Comment |
---|---|---|---|
Max. Thrust (wet) | kN | 90 | |
Max. Thrust (dry) | kN | 60 | |
Fuel Type | - | Jet A or JP8 | |
Power Supply Requirement | V | 28V | |
Power Take Off | - | ||
Fuel Pressure | Bar | ||
System Mass (dry) | kg | 991 | |
Fuel Mass Required 1000mph ISA day |
kg | 302 (390 litres) |
5mins idle,5 sec ramp to max dry, 5 sec max dry, 5 sec ramp to reheat, 41 sec reheat, controlled slam to idle. 5 mins idle Includes 10% ullage and allowance for scatter and deterioration of engine in line with RR worst case (Fuel mass based on RR Data, RA run profile May 2012 & 6.5T vehicle) |
Diameter | mm | 850 | |
Length | mm | 4000 |
EJ200 Intake Duct Specifications
Item | Unit | Target | Status | Comment |
---|---|---|---|---|
Intake Area | m2 | 0.28 – 0.38 | 0.35 | |
Aspect Ratio | - | 1.5 – 2.6 | 2 | |
Offset Ratio | - | 0.23 | 0.23 | |
Area Ratio | - | 0.8 | ||
Length | mm | 3.75 |
DISCLAIMER:
BLOODHOUND Programme Limited has provided this data as advisory and indicative and specifically and exclusively for the purpose of education. All facts, figures, concepts and principals provided relate only to the BLOODHOUND project. They may be inaccurate, out of date and subject to revision without notice. Under no circumstances should the data provided (or any derivative thereof) be used in whole or in part for any project, except in a purely theoretical environment. It should be understood that the entire project is experimental with high levels of personal risk and danger.
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