Liquid air cycle engine


Liquid air cycle engine

A liquid air cycle engine (LACE) is a spacecraft propulsion engine that attempts to gain efficiency by gathering part of its oxidizer from the atmosphere. In a LOX/LH2 bipropellant rocket the liquid oxygen needed for combustion is the majority of the weight of the spacecraft on lift-off, so if some of this can be collected from the air on the way, it might dramatically lower the take-off weight of the spacecraft.

Principle of operation

LACE works by compressing and then quickly liquefying the air. Compression is achieved through the ram-air effect in an intake similar to that found on a high-speed aircraft like Concorde, where intake ramps create shock waves that compress the air. The LACE design then blows the compressed air over a heat exchanger, in which the liquid hydrogen fuel is flowing. This rapidly cools the air, and the various constituents quickly liquefy. By careful mechanical arrangement the liquid oxygen can be removed from the other parts of the air, notably water, nitrogen and carbon dioxide, at which point it can be fed into the engine as normal. The hydrogen is so much lighter than oxygen that the now-warm hydrogen is often dumped overboard instead of being re-used as fuel, at a net gain.

One issue with the LACE system is that in order to appreciably reduce the mass of the oxygen carried at launch, a LACE vehicle needs to spend more time in the lower atmosphere where it can collect enough oxygen to supply the engines. This leads to greatly increased vehicle heating and drag, which offset somewhat the savings in oxidizer weight, but this in turn is offset by higher Isp (Specific impulse) permitting a lifting trajectory which greatly reduces gravity losses. More significantly the LACE system is far heavier than a rocket engine, and the performance of launch vehicles of all types is particularly affected by dry mass, rather than any oxidizer mass which would be burnt off over the course of the flight.

The advantages, or disadvantages, of the design continue to be a matter of some debate.

History

LACE was studied to some extent in the United States of America during the late 1950s and early 1960s, where it was seen as a "natural" fit for a winged spacecraft project known as the Aerospaceplane. At the time the concept was known as LACES, for "Liquid Air Collection Engine System", or ACES for "Air Collection and Enrichment System". Both Marquardt and General Dynamics were involved in the research, and by late 1960 Marquardt had a testbed system running that was capable of running a 275 lbf (1.2 kN) thrust engine for minutes at a time. However, as NASA moved to ballistic capsules during Project Mercury, funding for research into winged vehicles slowly disappeared, and LACE along with it.

imilar systems

LACE-like systems saw a brief re-emergence in England in 1982, when Alan Bond (formerly of the Blue Streak missile project) created a LACE-like design he called SATAN. The primary difference of these systems is that the air is only cooled, rather than liquified, and thus the gases are not actually separated, apparently giving significantly greater overall performance, due to a reduction in the amount of hydrogen used for cooling.

At the same time, John Scott and Bob Parkinson at British Aerospace had started some preliminary work on reusable launch systems. The two teams met and created HOTOL, which would use the BAe designed airframe with a Rolls Royce version of Bond's engine, known as the RB545. In 1986 the project was given an official go-ahead to the tune of 2 million pounds for research, but the program was later killed in 1989 when the project hit problems and the government refused further funding.

The principal designers then left to continue development on their own, but the RB545 had been classified top secret and could not be used. Instead Bond developed another version that is more advanced, known as SABRE (ostensibly for "Synergic Air BReathing Engine") which is meant for their Skylon design. Funding has not been terribly forthcoming (surprising, considering the design's potential to power an SSTO craft) and development continues at a relatively low level; papers and laboratory work are ongoing. A study of an aircraft powered by a SABRE class engine is underway under LAPCAT partially funded by the EU looking towards hypersonic intercontinental travel (Brussels to Sydney in 2-4 hours non stop).

ee also

*Air-augmented rocket
*RB545
*SABRE
*Scramjet
*Precooled jet engine

External links

* [http://www.sworld.com.au/steven/space/lace.txt Liquid Air Cycle Rocket Equation]
* [http://www.geocities.com/CapeCanaveral/Launchpad/6133/hotol.html HOTOL]


Wikimedia Foundation. 2010.

Look at other dictionaries:

  • Air-augmented rocket — Air augmented rockets (also known as rocket ejector, ramrocket, ducted rocket, integral rocket/ramjets, or ejector ramjets) use the supersonic exhaust of some kind of rocket engine to further compress air collected by ram effect during flight to… …   Wikipedia

  • Engine — This article is about a machine to convert energy into useful mechanical motion. For other uses of engine, see Engine (disambiguation). For other uses of motor, see Motor (disambiguation). A V6 internal combustion engine from a Mercedes car An… …   Wikipedia

  • Engine cooling — is cooling an engine, typically using either air or liquid.OverviewHeat engines generate mechanical power by extracting energy from heat flows, much as a water wheel extracts mechanical power from a flow of mass falling through a distance.… …   Wikipedia

  • Air-independent propulsion — (AIP) is a term that encompasses technologies which allow a submarine to operate without the need to surface or use a snorkel to access atmospheric oxygen. The term usually excludes the use of nuclear power, and describes augmenting or replacing… …   Wikipedia

  • Air-fuel ratio — (AFR) is the mass ratio of air to fuel present during combustion. When all the fuel is combined with all the free oxygen, typically within a vehicle s combustion chamber,the mixture is chemically balanced and this AFR is called the stoichiometric …   Wikipedia

  • Air conditioner — For general aspects of air conditioning, see Air conditioning. A typical home air conditioning unit. An air conditioner (often referred to as AC) is a home appliance, system, or mechanism designed to dehumidify and extract heat from an area. The… …   Wikipedia

  • Air conditioning — The term air conditioning refers to the cooling and dehumidification of indoor air for thermal comfort. In a broader sense, the term can refer to any form of cooling, heating, ventilation or disinfection that modifies the condition of air.… …   Wikipedia

  • Precooled jet engine — A precooled jet engine is a concept for high speed jet engines that features a cryogenic fuel cooled heat exchanger between the air intake and the (LP) compressor, to precool the air entering the compressor. After gaining heat and vapourising in… …   Wikipedia

  • Internal combustion engine — The internal combustion engine is an engine in which the combustion of a fuel (normally a fossil fuel) occurs with an oxidizer (usually air) in a combustion chamber. In an internal combustion engine, the expansion of the high temperature and high …   Wikipedia

  • Stirling engine — Alpha type Stirling engine. There are two cylinders. The expansion cylinder (red) is maintained at a high temperature while the compression cylinder (blue) is cooled. The passage between the two cylinders contains the regenerator …   Wikipedia


Share the article and excerpts

Direct link
Do a right-click on the link above
and select “Copy Link”

We are using cookies for the best presentation of our site. Continuing to use this site, you agree with this.