Difference between revisions of "Reaction engine"
(→Disadvantages) |
m (XZise moved page Rocket Engine to Rocket engine) |
(No difference)
| |
Revision as of 18:36, 10 June 2013
A rocket engine is an engine that uses nothing but its onboard propellant to generate thrust. Unlike traditional air breathing engines used by atmospheric crafts rocket engines are able to function in a vacuum where no oxygen is present.
Contents
History
Rocket engines were present in KSP in all public releases of the game.
Approaches to Rocket Engines
Rocket engines come in two commonly used forms. The first and most ancient type is a solid fuel rocket which is as simple as igniting a solid, self-oxidizing compound within the casing of the rocket and allowing the escaping gases to be released through a nozzle at the rear.
Liquid fuel engines are powered by a liquid propellant which is usually comprised of two separate fuels which are combined and ignited, typically liquid hydrogen and liquid oxygen or liquid kerosene, and liquid oxygen. In KSP there are two different types of liquid rocket engines; aerospike and bell type liquid rocket engines.
Solid Fuel Rocket Engines
Advantages
- Have a very high thrust to weight ratio.
- Engine and fuel tank are combined in one part, lowering part count, simplifying design and improving stability.
Disadvantages
- Monolithic design, must be built in one piece.
- Cannot be throttled or switched off after ignition.
- Once spent, they are unable to use fuel from another source of the craft.
Liquid Fuel Rocket Engines
Advantages
- Modular design: Fuel and other components can be stored elsewhere in the craft.
- Throttle can be adjusted depending on thrust requirements.
- Can be switched off and re-ignited at will.
- Many nozzles can be gimballed for thrust vectoring.
Disadvantages
- Lower power to weight ratio compared to Solid Rocket Engines.
- Complex design with fuel tanks and other additional components.
- More points of possible failure such as if the parts tear apart from stress.
- Efficiency largely dependent on design, with large variations.
