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The Bloodhound Project Propulsion - Jet

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 They may be inaccurate, out of date and subject to revision without notice.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.

BLOODHOUND Programme Limited, its directors, designers and associates do not accept any responsibility or liability whatsoever for use by any party of the data provided in breach of these terms.

All data provided by BLOODHOUND Programme Limited is confidential and proprietary to the BLOODHOUND Programme Limited. All such data shall only be used for the purposes of education and shall not be used by any party for commercial gain.