How Ramjets Work

By: Nicholas Gerbis  | 
NASA engineer Laura O'Connor inspects a supersonic ramjet (scramjet) engine model at Langley Research Center in Hampton, Virginia.
© Corbis
Key Takeaways
  • A ramjet is a type of air-breathing jet engine that operates on the principle of compressing incoming air without the need for rotating parts.
  • It relies on the high-speed forward motion of the aircraft to compress air, making it suitable for supersonic and hypersonic flight.
  • Ramjets are efficient at high speeds but require other propulsion systems for takeoff and acceleration, due to their inability to produce thrust at low speeds.

As anyone who's ever belly flopped off a high dive can tell you, when you hit a fluid without giving it time to get out of the way, it tends to hit back. Divers beat physics by taking a more streamlined plunge, and faster cars and aircraft do it by sporting more aerodynamic shapes. But there comes a point, near the sound barrier, where streamlining is not enough -- a speed at which the very air that keeps your plane aloft begins to hammer you with seemingly insurmountable drag, teeth-rattling turbulence and brutal shock waves. Indeed, many believed this sound barrier unbreakable until, on Oct. 14, 1947, Chuck Yeager's rocket-powered Bell X-1 proved them wrong.

But what if you could turn all that piled-up air to your advantage? What if, instead of churning through it with propellers or burning through it with rockets, you could pack it into a specially shaped tube, pump it up with an explosion and fire it out a nozzle at supersonic speeds, all with no major moving parts? You'd have a very special type of jet engine, a "flying stovepipe" fit for slicing through the sky at thousands of miles per hour. You'd have a ramjet.

Advertisement

But the ramjet's apparent simplicity is deceptive; it takes cutting-edge aeronautical engineering, modern materials and precision manufacturing to pull one off -- which partly explains why an idea nearly as old as powered flight was repeatedly taken up and cast aside for decades before achieving limited success during the Cold War.

Unlike its main speed competition, the rocket, which burns fuel using onboard oxidizers like ammonium nitrate, potassium chlorate or ammonium chlorate, ramjets breathe air. Thus, while rockets can operate in the near vacuum of space, ramjets must fly through the atmosphere. They must do so at very high speeds, too -- around Mach 2.5-3.0, or three times the speed of sound -- because ramjets work by harnessing ram pressure, the natural air compression brought on by an aircraft's high speed. In other words, ramjets make allies of the very shock waves and compression forces that once opposed high-speed flight; they literally go with the flow [sources: Encyclopaedia Britannica; NASA].

Ramjets are more efficient over long distances than rockets but suffer a significant disadvantage: They are useless at low velocities. Consequently, they rely on booster rockets or other vehicles to get them up to speed. Standalone ramjet aircraft typically use hybrid engines [source: NASA].

If that explanation flew past you at supersonic speed, it's probably because we skipped over a lot of cool and interesting stuff. Let's look at how jet engines have developed to produce this modern marvel.

Advertisement

Detonations and Arrivals

A cameraman with a high-speed camera films the thrust augmentor flame of a ramjet I-40 engine at the Lewis Flight Propulsion Laboratory in Cleveland. (The lab later became known as the John Glenn Research Center.)
© Corbis

Jets run on controlled explosions. That sounds strange until you realize that most car engines do, too: Pull in air, compress it, mix it with fuel, ignite it and bang! You've pushed a piston. But whereas gasoline and diesel engines involve cyclical or intermittent combustion, jets entail continuous combustion, in which fuel and air mix and burn nonstop. Either way, burning more rubber means guzzling more gas, and that means sucking in more oxygen to get the mixture right. Souped-up cars do this with superchargers; in jet engines, it's more complicated [source: Encyclopaedia Britannica].

The first operational jet aircraft zoomed into combat near the end of World War II using turbojet engines, a straightforward but ingenious design based on the Brayton (or Joule) Cycle: As the plane flies, air streams through an intake into a diffuser, a chamber that slows airflow and inhibits shock waves. It then passes through a series of bladed disks: spinning rotors, which force air backward, and stationary stators, which guide airflow. Together, they act as a compressor that pumps up pressure within the jet's combustion chambers. There, fuel mixes with pressurized air and ignites, blasting temperatures into the 1800-2800 F (980-1540 C) range or higher [sources: Encyclopaedia Britannica; Krueger; Spakovszky].

Advertisement

Pressure rises with temperature, so this explosion creates a lot of force with nothing to do but seek a quick exit. As the exhaust shoots through the rear nozzle it generates thrust to move the aircraft. En route to this nozzle, the exhaust also shoots through a turbine connected to the rotors by a torque shaft. As the turbine spins, it transfers energy to the compressor blades in front, completing the cycle.

In airplanes with turboprops or helicopters with turboshaft engines, the turbines also transfer power to a propeller or helicopter rotor via a series of gears.

Turbojets pack a lot of power but struggle at low speeds. Consequently, in the 1960s and 1970s, low-supersonic aircraft began trending toward the turbofans that most private jets and commercial airliners still use. A turbofan is the turducken of engines -- essentially a turbojet wrapped in a larger cowling with a big fan slapped on its front. The fan pulls in more air, which the engine then splits into two streams: Some air moves through the nested turbojet, while the rest flows through the empty space around it. The two streams reunite when redirected cooler air mixes with the turbojet's exhaust and slows it down, creating a larger, slower thrust stream that is more efficient at low speeds [sources: Encyclopaedia Britannica; Krueger].

Meanwhile, around the time that turbofans came into their own, research into ramjet aircraft was finally hitting its stride. It had been a long road.

Advertisement

Ramjets, Ahead of Their Time?

Whoever said that you have to walk before you can run never met Frenchman René Lorin. He saw the possibilities of ram-pressure propulsion as early as 1913, when pilots were still flying glorified wooden kites. Aware of the design's uselessness at subsonic speeds, he instead designed a ramjet-assisted flying bomb. The French military waved him off. Hungarian engineer Albert Fono, another ramjet pioneer, pursued a similar idea in 1915 and received a comparable reception from the Austro-Hungarian Army [sources: Gyorgy; Heiser and Pratt; Wolko].

Ramjets designs enjoyed a short vogue between world wars. Soviet engineers made early strides in rocket-based ramjets (see next section), but interest burned out before 1940. The German occupation interrupted French engineer René Leduc's early work, but his persistence and secrecy paid off on April 21, 1949, when his Lorin-inspired 010 model made its first powered flight of a ramjet aircraft. Carried aloft atop a Languedoc 161 airliner, it flew for 12 minutes and reached 450 mph (724 kph) at half power [sources: Siddiqi; Ward; Wolko; Yust et al.].

Advertisement

And, for a while, that was that. Despite Leduc's success, lack of funds ended official support for his research in 1957 [sources: Siddiqi; Ward; Wolko; Yust et al.]. The ramjet was beginning to look like an invention with no application. Meanwhile, World War II had ushered in the first generation of operational turbojets: the British Gloster Meteor, the German Messerschmitt Me 262 and the American Lockheed F-80 Shooting Star [sources: Encyclopaedia Britannica; Encyclopaedia Britannica; Encyclopaedia Britannica; National Museum of the USAF; van Pelt].

As the war ended and the Cold War heated up, it became clear that turbojets and turbofans presented more practical subsonic and low-supersonic solutions than ramjets. Thereafter, most U.S. and Soviet work in ramjets focused on building intercontinental missiles. In 1950, American engineer William H. Avery and the Johns Hopkins University Applied Physics Laboratory produced Talos, the U.S. Navy's first ramjet missile. Future generations would refine and streamline the design, introducing hybrid ramrockets capable of achieving high supersonic speeds (Mach 3-5) (see next section) [sources: Hoffman; Kossiakoff; Ward].

Despite intriguing designs like the Hiller XHOE-1 Hornet helicopter, the proposed Republic XF-103 bomber interceptor and the short-lived Lockheed D-21B unmanned reconnaissance drone, ramjet aircraft languished until the 1964 debut of the Lockheed SR-71 Blackbird. The fastest manned aircraft until its retirement in 1989, the Mach 3+ Blackbird also used a hybrid engine, sometimes called a turboramjet [sources: National Museum of the USAF; Smithsonian; Ward].

We'll dive into the SR-71 and other ramjet hybrids and subtypes in the next section.

Advertisement

Ramjets: Making Mock of Mach

The Lockheed SR-71A Blackbird reconnaissance aircraft prepares for flight. The Blackbird parked at the Steven F. Udvar-Hazy Center once flew from Los Angeles to Washington, D.C., in one hour, four minutes and 20 seconds.
© George Hall/Corbis

If ramjets are so fiddly, then why bother? Well, at the pressures and temperatures generated at Mach 2.5+, most jet engines become hugely impractical -- and utterly pointless. Even if you could make one work, doing so would combine the hazards of running a windmill in a hurricane with the pointlessness of hauling a wave machine to Oahu's North Shore.

Ramjets take the basic principles of other jets and crank them up to 11, all without major moving parts. Air enters a ramjet's diffuser at supersonic speeds, assaulting it with shock waves that help build ram pressure. A diamond-shaped center body in the intake further squeezes the air and slows it to subsonic speeds to more efficiently mix with fuel and combust. Combustion occurs in an open chamber akin to a giant afterburner, where liquid fuel is injected or solid fuel is ablated from the chamber's sides [sources: Ashgriz; Encyclopaedia Britannica; SPG; Ward].

Advertisement

Ramjets' speed limitations gradually inspired hybrid engines that could fly at lower speeds and accelerate to supersonic velocities. The most famous example, the SR-71 Blackbird, used a turbojet-ramjet hybrid called, appropriately, a turboramjet. Such engines work like an afterburning turbojet until well past Mach 1, after which ducts bypass the turbojet and redirect the ram-compressed airflow into the afterburner, making the engine behave like a ramjet [source: Ward].

Missile designs, meanwhile, gradually did away with boosters by moving them inside the ramjet itself, creating ramrockets, aka integral rocket ramjets. During rocket acceleration, plugs temporarily seal the ramjet's intake and fuel injectors. Once the rockets are spent and the ramjet is up to speed, these pop off, and the empty rockets act as combustion chambers [source: Ward].

Looking forward, crossing the Mach 5 line into hypersonic speeds will likely entail scramjets (supersonic combusting ramjets). Unlike other ramjets, scramjets do not need to slow air to subsonic speeds in their combustion chambers. To pull off ignition and expansion in the 0.001 seconds before the pressurized air shoots out the exhaust, scramjets typically use hydrogen fuel, which has a high specific impulse (change in momentum per unit mass of propellant), ignites over a wide range of fuel/air ratios and releases a huge burst of energy when burned [sources: Bauer; Encyclopaedia Britannica; NASA].

Scramjets remained theoretical before the past few decades, and work remains mostly experimental. In November 2004, NASA's eight-year, $230-million Hyper-X Program produced a scramjet that reached Mach 9.6 on its final flight. Some analysts believe the technology could reach Mach 15-24, but air travel at hypersonic speeds means overcoming forces unlike those faced by even the fastest supersonic craft. In short, we have a long way to go before we can commute from New York to Los Angeles in 12 minutes [sources: Bauer; DARPA; Fletcher; NASA].

Advertisement

Frequently Asked Questions

What are the limitations of ramjets in terms of speed?
Ramjets are efficient at high speeds but become less effective at lower speeds, requiring alternative propulsion systems for takeoff and acceleration.
How do ramjets differ from turbojets and turbofans in terms of operation?
Ramjets differ from turbojets and turbofans in that they do not have rotating compressor blades. Instead, they rely on the forward motion of the aircraft to compress air, making them more suitable for supersonic and hypersonic flight.

Lots More Information

Author's Note: How Ramjets Work

I'm often enchanted by stories of great innovations that failed to find an application when they were first invented. While writing this article, for example, I was repeatedly reminded of the laser, which was once called a solution looking for a problem.

Oh, what a difference a few decades make.

On the other hand, sometimes weird inventions make millions. Other times we invent things for one purpose that turn out to have unforeseen applications. Among its many contributions, the American space program invented the ribbed swimsuit and changed diapers forever. Today, materials scientists are discovering properties for which we have yet to find uses. With luck, they'll fare better than Lorin.

Related Articles

  • Ashgriz, Nasser. "Lecture 5: Inlets." Mechanical and Industrial Engineering, University of Toronto. (May 22, 2014) http://www.mie.utoronto.ca/labs/mfl/propulsion/lectures/lecture5/inlets.htm
  • Bauer, Daniel. "Scramjet Fuels: Hydrogen vs. Hydrocarbons." Journal of UNSW@ADFA Undergraduate Hypersonics, Vol. 1, No 1 (2007). (May 21, 2014) http://seit.unsw.adfa.edu.au/ojs/index.php/Hypersonics/article/view/18/8
  • Defense Advanced Research Project Agency (DARPA). "Falcon HTV-2 Three Key Technical Challenges." (May 29, 2014) http://www.darpa.mil/Our_Work/TTO/Falcon_HTV-2_Three_Key_Technical_Challenges.aspx
  • Encyclopaedia Britannica. "Ernst Heinrich Heinkel." (May 29, 2014) http://www.britannica.com/EBchecked/topic/259700/Ernst-Heinrich-Heinkel
  • Encyclopaedia Britannica. "History of Flight: The Jet Age." (May 29, 2014) http://www.britannica.com/EBchecked/topic/210191/history-of-flight/260590/The-jet-age
  • Encyclopaedia Britannica. "Internal Combustion Engine." (May 19, 2014) http://www.britannica.com/EBchecked/topic/290504/internal-combustion-engine
  • Encyclopaedia Britannica. "Jet Engine." (May 19, 2014) http://www.britannica.com/EBchecked/topic/303238/jet-engine
  • Encyclopaedia Britannica. "Military Aircraft: The Jet Age." (May 29, 2014) http://www.britannica.com/EBchecked/topic/382295/military-aircraft/57508/The-jet-age
  • Encyclopaedia Britannica. "Ramjet." (May 19, 2014) http://www.britannica.com/EBchecked/topic/490671/ramjet
  • Fletcher, D. G. "Fundamentals of Hypersonic Flow -- Aerothermodynamics." RTO AVT Lecture Series on Critical Technologies for Hypersonic Vehicle Development, the von Kármán Institute, Belgium, May 10-14, 2004. (May 21, 2014) http://ftp.rta.nato.int/public//PubFullText/RTO/EN/RTO-EN-AVT-116///EN-AVT-116-03.pdf
  • Gyorgy, Nagy Istvan. "Albert Fono: A Pioneer of Jet Propulsion." In Rocketry & Astronautics: IAC History Symposia 1967-2000 Abstracts & Index. Page 136. 2004. (May 22, 2014) http://iaaweb.org/iaa/Studies/history.pdf
  • Heiser, William H. and David T. Pratt. "Hypersonic Airbreathing Propulsion." AIAA. 1994.
  • Hoffman, Jascha. "William Avery, Jet Engine Scientist, Dies at 91." The New York Times. July 12, 2004. (May 22, 2014) http://www.nytimes.com/2004/07/12/us/william-avery-jet-engine-scientist-dies-at-91.html
  • Kossiakoff, Alexander. "In Memoriam: William H. Avery (1912–2004)." Johns Hopkins APL Technical Digest. Vol. 25, No. 2. Page 173. 2004. (May 22, 2014) http://techdigest.jhuapl.edu/techdigest/TD/td2502/avery.pdf
  • Krueger, Paul S. "Turbojets." Department of Mechanical Engineering, Southern Methodist University. (May 29, 2014) http://lyle.smu.edu/propulsion/Pages/jetengine.htm
  • Krueger, Paul S. "Variations of Jet Engines." Department of Mechanical Engineering, Southern Methodist University. (May 29, 2014) http://lyle.smu.edu/propulsion/Pages/variations.htm
  • Kumar, Satish, et al. "Scramjet Combustor Development." The Combustion Institute. (May 29, 2014) http://www.combustioninstitute-indiansection.com/pdf/SCRAMJET%20COMBUSTOR%20DEVELOPMENT.pdf
  • Long, K. F. "Deep Space Propulsion: A Roadmap to Interstellar Flight." Springer. 2012.
  • NASA. "Afterburning Turbojet." (May 30, 2014) https://www.grc.nasa.gov/www/k-12/airplane/aturba.html
  • NASA. "NASA Armstrong Fact Sheet: Hyper-X Program." Feb. 28, 2014. (May 21, 2014) http://www.nasa.gov/centers/armstrong/news/FactSheets/FS-040-DFRC.html#.U3zG0PldV8F
  • NASA. "NASA's Guide to Hypersonics." Oct. 21, 2008. (May 29, 2014) http://www.grc.nasa.gov/WWW/BGH/index.html
  • NASA. "Propellants." In Space Handbook: Astronautics and Its Applications. Staff Report of the Select Committee on Astronautics and Space Exploration. U. S. Government Printing Office. 1959. http://history.nasa.gov/conghand/propelnt.htm
  • NASA. "Warp Drive, When?" (May 30, 2014) http://www.nasa.gov/centers/glenn/technology/warp/warp.html
  • NASA. "What's a Scramjet?" Jan. 30, 2004. (May 21, 2014) http://www.nasa.gov/missions/research/f_scramjets.html
  • National Museum of the USAF. "Lockheed D-21B." Oct. 22, 2103. (May 29, 2014) http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=396
  • National Museum of the USAF. "Republic/Ford JB-2 Loon (V-1 Buzz Bomb)." Feb. 4, 2011. (May 29, 2014) http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=510
  • National Museum of the USAF. "Republic XF-103." Oct. 30, 2009. (May 29, 2014) http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2377
  • Oxford Dictionary of Science. "Jet Propulsion (Reaction Propulsion)." Isaacs, Alan, John Daintith and Elizabeth Martin, eds. Oxford University Press. 4th edition. 2003.
  • Pratt & Whitney. "F100 Engine." 2014. (May 29, 2014) http://www.pw.utc.com/F100_Engine
  • Siddiqi, Asif. "Challenge to Apollo: The Soviet Union and the Space Race 1945 - 1974." NASA SP-2000-4408. 2000. (May 22, 2014) http://history.nasa.gov/SP-4408pt1.pdf
  • Smithsonian National Air and Space Museum. "Hiller XHOE-1 Hornet." (May 29, 2014) http://airandspace.si.edu/collections/artifact.cfm?id=A19610115000
  • Space Propulsion Group. "Solid Fuel Ramjets." (May 22, 2014) http://www.spg-corp.com/solid-fuel-ramjets.html
  • Spakovszky, Z. S. "3.7 Brayton Cycle." From Unified: Thermodynamics and Propulsion. Massachusetts Institute of Technology. Aug. 6, 2006. (May 19, 2014) http://web.mit.edu/16.unified/www/SPRING/propulsion/notes/node27.html
  • van Pelt, Michel. "Rocketing into the Future." Springer Praxis Books. 2012.
  • Ward, Thomas A. Aerospace Propulsion Systems. Wiley. May 17, 2010.
  • Wolko, Howard S. "In the Cause of Flight: Technologists of Aeronautics and Astronautics." Smithsonian Studies in Air and Space Number 4. Smithsonian Institution Press. 1981.
  • Yest, Walter et al. "Jet Propulsion." Britannica Book of the Year 1950. Encyclopedia Britannica, Inc. 1950. (May 22, 2014) http://archive.org/stream/britannicabookof030518mbp/britannicabookof030518mbp_djvu.txt

Advertisement

Loading...