Bussard ramjet

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Artist's conception of a Bussard ramjet. A major component of an actual ramjet - a miles-wide electromagnetic field - is invisible. Bussard Interstellar Ramjet Engine.jpg
Artist's conception of a Bussard ramjet. A major component of an actual ramjet a miles-wide electromagnetic field is invisible.
Bussard ramjet in motion.
Interstellar medium
Collect and compress hydrogen
Transport hydrogen beside the payload
Thermonuclear fusion
Engine nozzle
Flue gas jet Bussard ramjet.gif
Bussard ramjet in motion.
  1. Interstellar medium
  2. Collect and compress hydrogen
  3. Transport hydrogen beside the payload
  4. Thermonuclear fusion
  5. Engine nozzle
  6. Flue gas jet

The Bussard ramjet is a theoretical method of spacecraft propulsion for interstellar travel. A fast moving spacecraft scoops up hydrogen from the interstellar medium using an enormous funnel-shaped magnetic field (ranging from kilometers to many thousands of kilometers in diameter); the hydrogen is compressed until thermonuclear fusion occurs, which provides thrust to counter the drag created by the funnel and energy to power the magnetic field. The Bussard ramjet can thus be seen as a ramjet variant of a fusion rocket.[ citation needed ]

Contents

The Bussard ramjet was proposed in 1960 by the physicist Robert W. Bussard. [1]

The concept was popularized by Poul Anderson in his novel Tau Zero , Larry Niven in his Known Space series of books, Vernor Vinge in his Zones of Thought series, and Carl Sagan, as referenced in the television series and book Cosmos .[ citation needed ]

Feasibility

Since the time of Bussard's original proposal, it has been discovered that the region surrounding the Solar System has a much lower density of hydrogen than was believed at that time (see Local Interstellar Cloud). In 1969, John Ford Fishback made an important contribution, describing the details of the required magnetic field. [2]

In 1978, T. A. Heppenheimer analyzed Bussard's original suggestion of fusing protons, but found the Bremsstrahlung losses from compressing protons to fusion densities was greater than the power that could be produced by a factor of about 1 billion, thus indicating that the proposed version of the Bussard ramjet was infeasible. [3] However, Daniel P. Whitmire's 1975 analysis [4] indicates that a ramjet may achieve net power via the CNO cycle, which produces fusion at a much higher rate (~1016 times higher) than the proton–proton chain.[ citation needed ]

Robert Zubrin and Dana Andrews analyzed one hypothetical version of the Bussard ramjet design in 1988. [5] They determined that their version of the ramjet would be unable to accelerate into the solar wind.[ citation needed ]

A 2021 study found that, while feasible in principle, the practical construction of a useful Bussard ramjet would be beyond even a civilization of Kardashev type II. [6] [7]

Ram Augmented Interstellar Rocket (RAIR)

The problem of using the interstellar medium as the sole fuel source led to study of the Ram Augmented Interstellar Rocket (RAIR). The RAIR carries its nuclear fuel supply and exhausts the reaction products to produce some of its thrust. However it greatly enhances its performance by scooping the interstellar medium and using this as extra reaction mass to augment the rocket. The propulsion system of the RAIR consists of three subsystems: a fusion reactor, a scoop field, and a plasma accelerator. Fuel is launched ahead of the ship with the accelerator. [8] The scoop field funnels the fuel into another accelerator (this could for example be a heat exchange system transferring thermal energy from the reactor directly to the interstellar gas) which is supplied power from a reactor. One of the best ways to understand this concept is to consider that the hydrogen nuclear fuel carried on board acts as a fuel (energy source) whereas the interstellar gas collected by the scoop and then exhausted at great speed from the back acts as a propellant (the reaction mass), the vehicle therefore has a limited fuel supply but an unlimited propellant supply. A normal Bussard ramjet would have an infinite supply of both. However, theory suggests that where a Bussard ramjet would suffer drag from having to pre-accelerate interstellar gas to its own speed before intake, a RAIR system would be able to transfer energy via the "accelerator" mechanism to the interstellar medium despite velocity differences, and so would suffer far less drag. [9] [10] [11] [12]

Laser Powered Interstellar Ramjet

Beamed energy coupled with a vehicle scooping hydrogen from the interstellar medium is another variant. A laser array in the solar system beams to a collector on a vehicle which uses something like a linear accelerator to produce thrust. This solves the fusion reactor problem for the ramjet. There are limitations because of the attenuation of beamed energy with distance. [13]

Magnetic sail

The calculations (by Robert Zubrin and Dana Andrews) inspired the idea of a magnetic parachute or sail. This could be important for interstellar travel because it means that deceleration at the destination can be performed with a magnetic parachute rather than a rocket. [14]

Dyson swarm-based stellar engine (Caplan thruster)

Astrophysicist Matthew E. Caplan of Illinois State University has proposed a type of stellar engine that uses a Dyson swarm of mirrors to concentrate stellar energy onto certain regions of a Sun-like star, producing beams of solar wind to be collected by a multi-ramjet assembly which in turn produces directed jets of plasma to stabilize its orbit and oxygen-14 to push the star. Using rudimentary calculations that assume maximum efficiency, Caplan estimates the Bussard engine would use 1015 grams per second of solar material to produce a maximum acceleration of 10−9 m/s2, yielding a velocity of 200 km/s after 5 million years, and a distance of 10 parsecs over 1 million years. The Bussard engine would theoretically work for 100 million years given the mass loss rate of the Sun, but Caplan deems 10 million years to be sufficient for a stellar collision avoidance. [15]

Pre-seeded trajectory

Several of the obvious technical difficulties with the Bussard ramjet can be overcome by setting out solid pellets of fuel along the spacecraft's trajectory in advance. [16] This could be done using a different "tanker" spacecraft dropping fuel pellets [16] [17] or using laser propulsion. [18] The method has been referred to as the "fusion runway", [16] [18] ramjet runway [17] or "forward resupply runway". [19]

While most proposals use fusion power, as with conventional Bussard ramjets, fission has also been suggested. [19]

The advantages of this system include:

The major disadvantages of this system include:[ citation needed ]

See also

Related Research Articles

<span class="mw-page-title-main">Interstellar travel</span> Hypothetical travel between stars or planetary systems

Interstellar travel is the hypothetical travel of spacecraft from one star system, solitary star, or planetary system to another. Interstellar travel is expected to prove much more difficult than interplanetary spaceflight due to the vast difference in the scale of the involved distances. Whereas the distance between any two planets in the Solar System is less than 55 astronomical units (AU), stars are typically separated by hundreds of thousands of AU, causing these distances to typically be expressed instead in light-years. Because of the vastness of these distances, non-generational interstellar travel based on known physics would need to occur at a high percentage of the speed of light; even so, travel times would be long, at least decades and perhaps millennia or longer.

<span class="mw-page-title-main">Interplanetary spaceflight</span> Crewed or uncrewed travel between stars or planets

Interplanetary spaceflight or interplanetary travel is the crewed or uncrewed travel between stars and planets, usually within a single planetary system. In practice, spaceflights of this type are confined to travel between the planets of the Solar System. Uncrewed space probes have flown to all the observed planets in the Solar System as well as to dwarf planets Pluto and Ceres, and several asteroids. Orbiters and landers return more information than fly-by missions. Crewed flights have landed on the Moon and have been planned, from time to time, for Mars, Venus and Mercury. While many scientists appreciate the knowledge value that uncrewed flights provide, the value of crewed missions is more controversial. Science fiction writers propose a number of benefits, including the mining of asteroids, access to solar power, and room for colonization in the event of an Earth catastrophe.

<span class="mw-page-title-main">Ramjet</span> Supersonic atmospheric jet engine

A ramjet is a form of airbreathing jet engine that requires forward motion of the engine to provide air for combustion. Ramjets work most efficiently at supersonic speeds around Mach 3 and can operate up to Mach 6.

<span class="mw-page-title-main">Spacecraft propulsion</span> Method used to accelerate spacecraft

Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites. In-space propulsion exclusively deals with propulsion systems used in the vacuum of space and should not be confused with space launch or atmospheric entry.

Beam-powered propulsion, also known as directed energy propulsion, is a class of aircraft or spacecraft propulsion that uses energy beamed to the spacecraft from a remote power plant to provide energy. The beam is typically either a microwave or a laser beam and it is either pulsed or continuous. A continuous beam lends itself to thermal rockets, photonic thrusters and light sails, whereas a pulsed beam lends itself to ablative thrusters and pulse detonation engines.

<span class="mw-page-title-main">Fusion rocket</span> Rocket driven by nuclear fusion power

A fusion rocket is a theoretical design for a rocket driven by fusion propulsion that could provide efficient and sustained acceleration in space without the need to carry a large fuel supply. The design requires fusion power technology beyond current capabilities, and much larger and more complex rockets.

<span class="mw-page-title-main">Antimatter rocket</span> Rockets using antimatter as their power source

An antimatter rocket is a proposed class of rockets that use antimatter as their power source. There are several designs that attempt to accomplish this goal. The advantage to this class of rocket is that a large fraction of the rest mass of a matter/antimatter mixture may be converted to energy, allowing antimatter rockets to have a far higher energy density and specific impulse than any other proposed class of rocket.

<span class="mw-page-title-main">Nuclear pulse propulsion</span> Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust

Nuclear pulse propulsion or external pulsed plasma propulsion is a hypothetical method of spacecraft propulsion that uses nuclear explosions for thrust. It originated as Project Orion with support from DARPA, after a suggestion by Stanislaw Ulam in 1947. Newer designs using inertial confinement fusion have been the baseline for most later designs, including Project Daedalus and Project Longshot.

<span class="mw-page-title-main">Spaceflight</span> Flight into or through outer space

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Robert W. Bussard was an American physicist who worked primarily in nuclear fusion energy research. He was the recipient of the Schreiber-Spence Achievement Award for STAIF-2004. He was also a fellow of the International Academy of Astronautics and held a Ph.D. from Princeton University.

<span class="mw-page-title-main">Nuclear propulsion</span> Nuclear power to propel a vehicle

Nuclear propulsion includes a wide variety of propulsion methods that use some form of nuclear reaction as their primary power source. The idea of using nuclear material for propulsion dates back to the beginning of the 20th century. In 1903 it was hypothesized that radioactive material, radium, might be a suitable fuel for engines to propel cars, planes, and boats. H. G. Wells picked up this idea in his 1914 fiction work The World Set Free. Many aircraft carriers and submarines currently use uranium fueled nuclear reactors that can provide propulsion for long periods without refueling. There are also applications in the space sector with nuclear thermal and nuclear electric engines which could be more efficient than conventional rocket engines.

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<span class="mw-page-title-main">Project Daedalus</span> 1970s proposal for a large fusion powered unmanned interstellar probe

Project Daedalus was a study conducted between 1973 and 1978 by the British Interplanetary Society to design a plausible uncrewed interstellar probe. Intended mainly as a scientific probe, the design criteria specified that the spacecraft had to use existing or near-future technology and had to be able to reach its destination within a human lifetime. Alan Bond led a team of scientists and engineers who proposed using a fusion rocket to reach Barnard's Star 5.9 light years away. The trip was estimated to take 50 years, but the design was required to be flexible enough that it could be sent to any other target star.

<span class="mw-page-title-main">Heliosphere</span> Region of space dominated by the Sun

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<span class="mw-page-title-main">Stellar engine</span> Class of hypothetical megastructures

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<span class="mw-page-title-main">Solar One (interstellar)</span>

Solar One is a proposed spacecraft that would combine beamed-powered propulsion, electromagnetic propulsion, and nuclear propulsion. The spacecraft would include a light sail, a laser system, a Bussard scoop, and a compact nuclear fusion reactor. Large mirrors would be assembled in orbit and sent close to the Sun to collect sufficient light to propel the light sail. The on board laser would help the Bussard scoop collect hydrogen to power the nuclear reactor which, in turn, would power both the laser and the electromagnetic scoop to decelerate the spacecraft. The main challenges are building large parabolic mirrors as well as reducing the weight of the on board laser system and compact nuclear reactor.

References

  1. Bussard, Robert W. (1960). Galactic Matter and Interstellar Flight (PDF). Astronautica Acta. Vol. 6. pp. 179–195. Archived from the original (PDF) on 2018-04-17. Retrieved 2014-10-04.
  2. Fishback, J. F. (1969). "Relativistic interstellar spaceflight". Astronautica Acta. 15: 25–35. Bibcode:1969AsAc...15...25F.
  3. Heppenheimer, T.A. (1978). "On the Infeasibility of Interstellar Ramjets". Journal of the British Interplanetary Society. 31: 222. Bibcode:1978JBIS...31..222H.
  4. Whitmire, Daniel P. (May–June 1975). "Relativistic Spaceflight and the Catalytic Nuclear Ramjet" (PDF). Acta Astronautica. 2 (5–6): 497–509. Bibcode:1975AcAau...2..497W. CiteSeerX   10.1.1.492.6775 . doi:10.1016/0094-5765(75)90063-6. Archived from the original (PDF) on 2018-10-31. Retrieved 2009-08-30.
  5. Andrews, D.G.; Zubrin, R.M. (1988). Magnetic sails and interstellar travel. 39th International Astronautical Congress, Bangalore. Art. IAF Paper IAF-88-533.
  6. Schattschneider, Peter; Jackson, Albert A. (February 2022). "The Fishback ramjet revisited". Acta Astronautica. 191: 227–234. Bibcode:2022AcAau.191..227S. doi: 10.1016/j.actaastro.2021.10.039 .
  7. Ouellette, Jennifer (January 6, 2022). "Study: 1960 ramjet design for interstellar travel—a sci-fi staple—is unfeasible". Ars Technica . Archived from the original on January 23, 2024.
  8. "Innovative Technologies from Science Fiction for Space Applications" (PDF). esa.it. p. 13. Archived (PDF) from the original on December 28, 2023. Retrieved May 2, 2023.
  9. Bond, A. (1974). "An Analysis of the Potential Performance of the Ram Augmented Interstellar Rocket". Journal of the British Interplanetary Society. 27: 674–688. Bibcode:1974JBIS...27..674B.
  10. Powell, C. (1976). "System Optimization for the Ram Augmented Interstellar Rocket". Journal of the British Interplanetary Society. 29 (2): 136. Bibcode:1976JBIS...29..136P.
  11. Jackson, A. (1980). "Some Considerations on the Antimatter and Fusion Ram Augmented Interstellar Rocket". Journal of the British Interplanetary Society. 33: 117–120. Bibcode:1980JBIS...33..117J.
  12. Further information on this RAIR concept can be found in the book "the star flight handbook" and at http://www.projectrho.com/public_html/rocket/slowerlight.php
  13. Whitmire, D.; Andrew Jackson (1977). "Laser Powered Interstellar Ramjet". Journal of the British Interplanetary Society. 30: 223–226. Bibcode:1977JBIS...30..223W.
  14. Perakis, N.; Andreas M. Hein (2016). "Combining Magnetic and Electric Sails for Interstellar Deceleration". Cornell University. 128: 13–20. arXiv: 1603.03015 . Bibcode:2016AcAau.128...13P. doi:10.1016/j.actaastro.2016.07.005. S2CID   17732634.
  15. Caplan, Matthew (December 17, 2019). "Stellar engines: Design considerations for maximizing acceleration". Acta Astronautica. 165: 96–104. Bibcode:2019AcAau.165...96C. doi:10.1016/j.actaastro.2019.08.027. S2CID   203111659. Archived from the original on December 23, 2019. Retrieved December 22, 2019. Alt URL
  16. 1 2 3 4 5 6 Discussed on Gilster, P. (2004). Centauri Dreams: Imagining and Planning Interstellar Exploration. Springer. pp.  146–8. ISBN   978-0-387-00436-5. Also in the entry 'A Fusion Runway to Nearby Stars' from centauri-dreams.org.
  17. 1 2 Matloff, Gregory L. (2006-08-31). Deep Space Probes: To the Outer Solar System and Beyond. Springer Science & Business Media. pp. 118–120. ISBN   978-3-540-27340-0.
  18. 1 2 "Bussard buzz-bomb (Jordin Kare)". yarchive.net. Retrieved 2024-01-22.
  19. 1 2 Lenard, Roger X.; Lipinski, Ronald J. (January 19, 2000). "Interstellar rendezvous missions employing fission propulsion systems". AIP Conference Proceedings. 504 (1). American Institute of Physics: 1544–1555. doi:10.1063/1.1290979. ISSN   1551-7616.
  20. Wang, Brian (June 20, 2017). "Nuclear fusion pellet runway". nextbigfuture.com. Archived from the original on January 23, 2024. Retrieved January 22, 2024.

Bibliography