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Expander cycle (rocket)



 

Additional recommended knowledge

The expander cycle is a power cycle of a bipropellant rocket engine meant to improve the efficiency of fuel delivery.

In an expander cycle, the fuel is heated before it is combusted, usually with waste heat from the main combustion chamber. As the liquid fuel passes through coolant passages in the walls of the combustion chamber, it undergoes a phase change into a gaseous state. The expansion of the fuel can create pressures of over 1000 psi (7 MPa) [1], which is used to drive turbines that in turn supply more fuel and oxidizer to the rocket engine. After leaving the turbines, the fuel is then burned to produce thrust for the vehicle.

Because of the necessary phase change, the expander cycle is thrust limited by the square cube rule. In bell shaped rockets there is a point beyond which there isn't enough nozzle area to heat up enough fuel to drive the turbines and hence the fuel pumps. In bell shaped rockets the expander cycle is limited to engines with up to 300 kN thrust. In aerospike shaped engines the exhaust effectively sticks to the aerospike, and can achieve a much higher heat transfer, and hence achieve greater thrust. Both engine types need to use a cryogenic fuel such as hydrogen, methane, or propane, which can easily reach their boiling point.

Expander cycle usually used a gas generator of some kind to start the turbine and run the engine until it heats up enough for phase change pressure to take over.

In an open cycle, or "bleed" expander cycle, only some of the fuel is heated to drive the turbines, which is then vented to atmosphere to increase turbine efficiency. While this increases power output, the dumped fuel leads to decreased efficiency. A closed cycle expander engine sends the turbine exhaust to the combustion chamber (see image at right.)

The expander cycle has a number of advantages:

  • Low temperature. The advantage is that after they have turned gaseous, the fuels are usually near room temperature, and do very little or no damage to the turbine, allowing the engine to be reusable. In contrast Gas-generator or Staged combustion engines operate their turbines at high temperature. The SSME destroys its turbines after each flight[citation needed]).
  • Tolerance. During the development of the RL-10 engineers were worried that insulation foam mounted on the inside of the tank might break off and damage the engine. They tested this by putting loose foam in a fuel tank and running it through the engine. The RL-10 chewed it up without problems or noticeable degradation in performance. Conventional gas-generators are in practice miniature rocket engines, with all the complexity that implies. Blocking even a small part of a gas generator can lead to a hot spot, which can cause violent loss of the engine. Using the engine bell as a 'gas generator' also makes it very tolerant of fuel contamination because of the wider fuel flow channels used.
  • Inherent safety. Because a bell-type expander-cycle engine is thrust limited, it can easily be designed to withstand its maximum thrust conditions. In other engine types, a stuck fuel valve or similar problem can lead to engine thrust spiraling out of control due to unintended feedback systems. Other engine types require complex mechanical or electronic controllers to ensure this does not happen. Expander cycles are by design incapable of malfunctioning that way.

Some examples of an expander cycle engine are the Pratt & Whitney RL-10 (rocket engine) and RL60 [2] and the Ariane 5 ESC-B [3].

Usage

Expander cycle engines include the following:

  • Pratt & Whitney RL-10
  • Pratt & Whitney RL-60
  • Vinci

Expander cycle engines have been used in:

  • Centaur upper stage
  • DC-X Arguably the world's first functionally reusable rocket.
  • Ariane 5 upper stage
  • Saturn I

See also

 
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Expander_cycle_(rocket)". A list of authors is available in Wikipedia.
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