Overall design of satellite launcher has been chosen to make maximum use of components and design concept of Black Knight; to save cost, size of vehicle and supporting service requirements have been tailored to existing Black Knight facilities in Great Britain and Australia; Black Arrow consists of three stages, first and second stages using liquid propellants hydrogen-peroxide and kerosene; third stage is spin-stabilized solid-propellant motor; other details and possible missions.
Black arrow
Flight
Flight International ; 90 , n 2994
1966
Article (Journal)
English
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Engineering Index Backfile | 1967
|NTIS | 1969
|Black arrow satellite launching vehicle
Engineering Index Backfile | 1968
|The Black Arrow Control System
NTIS | 1968
|The Black Arrow Satellite Launching Vehicle
NTIS | 1968
|