LOGIN   |  CONTACT US   |  NEWSLETTER

Vehicle Technical Specification - Part 3

10      VEHICLE PERFORMANCE

[Issue 8; Configuration 10; 10th May 2010]

10.1      Acceleration/Velocity

Definition Unit Target Status
10th May 2010
Status
Package Freeze
Status
Drawing Release
Comment
Velocity av. of 2 runs in opposite direction over measured mile. mph >1000       To FIA regulations.
Acceleration distance mile <4.5       Total track distance 10 mile
Max Velocity (Vmax) mph 1050       Or as appropriate to achieve the above average speed

 

10.2      Vehicle Braking

Definition Unit Target Status
10th May 2010
Status
Package Freeze
Status
Drawing Release
Comment
Available Track Braking Distance Miles ≥5.5 5.5     Hakskeen Pan: 10 mile track plus 1 mile of over run at each end
Nominal distance: Vmax to 0 mph   4.5 ?     ‘chute solution TBD
Airbrake
Max Deployment Speed mph 800 800      
Max Deceleration g 3 3     Progressive deployment to maintain g for as long as possible
Braking Distance miles 4.5 >4.5     Airbrake-only braking dist, no chutes
Parachute
Number of Parachutes   2 2     Target: 2 identical chutes, chute 2 as spare for chute 1
Parachute 1 (fully reefed)
Max Deployment Speed mach 0.9 0.9     Max strop load TDB
Max Deceleration g 3 3      
Parachute 2 (unreefed)
Max Deployment Speed mph 400 ?     TBD
Max Deceleration g 3 3      
Friction Brake
Application speed mph <250       Modified twin rotor DieselMax brake to be verified against the targets
Pedal Effort @ 1g N <500        
Pedal Travel @ 1g mm <100        
Brake Fade (Increase in effort) % <5        
Deceleration (g) g 1 (Tarmac) 0.3 (Alkali)        

 

10.3      Aerodynamics

Definition Unit Target Status
10th May 2010
Status
Package Freeze
Status
Drawing Release
Comment
Frontal Area m2   1.937      
M=0.5 Coefficient of Drag Area Cda 0.5 1.1      
M=0.7 Coefficient of Drag Area Cda 0.7 1.13      
M=1.0 Coefficient of Drag Area Cda <1.3 1.28      
M=1.4 Coefficient of Drag Area Cda <1.3 1.32      
M=0.5 Coefficient of Lift Cl   -0.38      
M=0.7 Coefficient of Lift Cl   -0.08      
M=1.0 Coefficient of Lift Cl   0.3      
M=1.4 Coefficient of Lift Cl   0.3      
Yaw Static Margin at M=1.3 % 3% - 5% ?      
Front downforce percentage of static contact patch force % 0 to 5        
Rear downforce percentage of static contact patch force % 5 to 10        

 

 [back to contents]

 

11      AUXILIARY POWER UNIT (APU) and HTP DELIVERY SYSTEM

[Issue 8; Configuration 10; 10th May 2010]

11.3      HTP Pump Specification

Definition Unit Target Status
10th May 2010
Status
Comment
Pump Configuration         Stentor large pump with improved volute
Power Requirement (Design) shp 665 665    
Peak Pump Speed (Contingency) rpm 12000 12000    
Pump Speed (Design) rpm 11000 11000    
Pump Torque (Design) Nm 430 430    
Pump Flow Rate (Design) kg/sec 47.6 47.6    
HTP Inlet Pressure MPa 0.165 0.165    
HTP Delivery Pressure (Design) MPa 7.58 7.58    
Volute and Bearing Housing -       Aluminium
Pump Shaft, Impeller & Inducer -       Stainless Steel
Front/rear Bearing Type -       Roller/Ball Race
Pump Cooling -       Self cooling with HTP
Pump Mass kg   34    

 

11.4      HTP Tank Specification

Definition Unit Target Status
10th May 2010
Status
Comment
Tank Configuration         TBC
Total Tank Volume litres 810 963    
Dimensions mm TBC TBC    
Material   6061 T6 Aluminium Teflon/Carbon filament wound    
Working Pressure MPa 0.165 0.165    
Max. Working Temperature ˚C As low as possible ?    
Test Pressure MPa TBC TBC    
Baffle Configuration         Horizontal and vertical plates with 114mm diam holes
Outlet Diameter mm 108 108    
Pressurising Gas   Nitrogen Nitrogen    
Vent Valve diameter mm 100-150 100-150   Needs rubber hose connection
Combined fill and drain mm ? ?   Situated on top of tank – internal pipe extending from top to bottom
Water Port mm ? ?   For tank flooding in an emergency
Leak Mitigation Mechanism         Tank covered in external plastic jacket to contain small leaks

 

 [back to contents]

 

12      VEHICLE STABILITY TARGETS

[Issue 8; Configuration 10; 10th May 2010]

Definition Unit Target Status
10th May 2010
Status
Package Freeze
Status
Drawing Release
Comment
Static Stability Index (Design Condition full with Fluids and Driver) G >1 1.025      
Static Stability Index (Empty and Driver) G >1 1.021      
Dynamic Stability Index (Design Condition full with Fluids and Driver) G >0.83 0.75     a.b/k^2 . where a & b are distance to axles from C of G, k is radius of gyration
Dynamic Stability Index (Empty and Driver) G >0.83 0.75     a.b/k^2 . where a & b are distance to axles from C of G, k is radius of gyration
Yaw Static Margin Aerodynamic (Design Condition full with Fluids and Driver) % 3 to 5 ?     Percentage of wheelbase
Yaw Static Margin Aerodynamic (Empty and Driver) % 3 to 5 ?     Percentage of wheelbase
Static Margin Vehicle Dynamic (Design Condition full with Fluids and Driver) % 5 to 10 5 est     Percentage of wheelbase
Static Margin Vehicle Dynamic (Empty and Driver) % 5 to 10 0 est     Percentage of wheelbase
Yaw Velocity Overshoot % 4 ?      
Roll Gain deg/g <4 2.64      
Rollover Resistance G ≥0.8       Target supported by CFD study of Thrust SSC lateral G scenario using current CFD code.

 

 [back to contents]

 


 

Part 1 ¦ Part 2 ¦ Part 3 ¦ Part 4 ¦ Part 5 ¦ Part 6

© BLOODHOUND Programme Ltd 2012 All Rights Reserved. BLOODHOUND SSC ® is a European Registered Trade Mark
Powered by scenta | Terms & Conditions | Disclaimer on use of information and data