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Typical fuel combinations are liquid hydrogen and oxygen (called hydrolox) and kerosine plus liquid oxygen (kerolox).
 
Typical fuel combinations are liquid hydrogen and oxygen (called hydrolox) and kerosine plus liquid oxygen (kerolox).
  
===Solid rocket===
 
[[Image:SolidRocket.png|thumb|left|100px|Solid rocket]]
 
 
A solid rocket or solid rocket motor stores all the propellants in solid form inside the [[Combustion chamber|combustion chamber]]. Their advantage is, that, once ignited, they don't shutdown. They are also very simple in design and construction and can deliver very high thrust. Their main disadvantage are their low [[specific impulse]].
 
 
 
Once ignited, thrust can only be terminated by thrust termination devices, which for example lower the chamber pressure below the threshold required for sustaining combustion. This is usually destructive.
 
 
[[Category: Articles]]
 
 
[[Category:Glossary]]
 
[[Category:Glossary]]

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