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The Bloodhound Project Geometric Datums

Bloodhound SSC Vehicle Technical Specification: configuration 11, June 2012

 

X, Y, Z co-ordinates for the position of Major Components/Assemblies*:

 

Definition Unit Target Status Comment
Parachutes mm      
Rear Wheels/suspension mm   15900,0,635 WHEEL CENTRE ,X,Y,Z
Rear Stabiliser mm      
Rocket engine & casing mm   16436.95,0,737.3808 REAR FACE OF ROCKET NOZZLE X,Y,Z ROCKET 2 DEGREES NOSE DOWN
Eurojet EJ200 mm   12406.75,0,1570 FRONT FACE OF JET X,Y,Z
CHASSIS COCKPIT SPLIT mm   X=10185  
TOP AND BOTTOM CHASSIS SPLIT mm   Z=1042  
Rear structure and skins mm      
EJ200 intake structure mm      
APU Assy mm      
HTP Tank mm      
Driver/cockpit structure mm      
Front wheels mm   7000,0,635 CENTRE OF WHEEL X,Y,Z
Front stabiliser mm      
APU Cooling system mm      
Nose Structure mm      

 

*All X,Y,Z coordinates refer to vehicle datum as per BLOODHOUND Design Office Standards:

x=0 at 7000mm ahead of front axle centreline

y=0 at mid-point of wheel track

z=0 at 200mm below ground level

 


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