请输入您要查询的百科知识:

 

词条 Liquid oxygen
释义

  1. Physical properties

  2. Uses

      In rocket propellant  

  3. History

  4. See also

  5. References

{{About|the liquid form of the element oxygen|the commercial dietary supplement product|Liquid Oxygen (supplement)}}{{Redirect|LOX||Lox (disambiguation)}}

Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is the liquid form of elemental oxygen. It was used as the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard[1]. It was later mostly supplanted by gaseous oxidizers such as nitrogen tetroxide because of easier storage, as is the case with the American Titan II missile from the Cold War.

Physical properties

Liquid oxygen has a pale blue color and is strongly paramagnetic: it can be suspended between the poles of a powerful horseshoe magnet.[2] Liquid oxygen has a density of 1.141 g/cm3 (1.141 kg/L or 1141 kg/m3), slightly denser than liquid water, and is cryogenic with a freezing point of {{convert|54.36|K|abbr=on}} and a boiling point of {{convert|90.19|K|abbr=on}} at 101.325 kPa (760 mmHg). Liquid oxygen has an expansion ratio of 1:861 under {{convert|1|atm|lk=on}} and {{convert|20|°C|abbr=on}},[3][4] and because of this, it is used in some commercial and military aircraft as a transportable source of breathing oxygen.

Because of its cryogenic nature, liquid oxygen can cause the materials it touches to become extremely brittle. Liquid oxygen is also a very powerful oxidizing agent: organic materials will burn rapidly and energetically in liquid oxygen. Further, if soaked in liquid oxygen, some materials such as coal briquettes, carbon black, etc., can detonate unpredictably from sources of ignition such as flames, sparks or impact from light blows. Petrochemicals, including asphalt, often exhibit this behavior.[5]

The tetraoxygen molecule (O4) was first predicted in 1924 by Gilbert N. Lewis, who proposed it to explain why liquid oxygen defied Curie's law.[6] Modern computer simulations indicate that although there are no stable O4 molecules in liquid oxygen, O2 molecules do tend to associate in pairs with antiparallel spins, forming transient O4 units.[7]

Liquid nitrogen has a lower boiling point at −196 °C (77 K) than oxygen's −183 °C (90 K), and vessels containing liquid nitrogen can condense oxygen from air: when most of the nitrogen has evaporated from such a vessel there is a risk that liquid oxygen remaining can react violently with organic material. Conversely, liquid nitrogen or liquid air can be oxygen-enriched by letting it stand in open air; atmospheric oxygen dissolves in it, while nitrogen evaporates preferentially.

Uses

In commerce, liquid oxygen is classified as an industrial gas and is widely used for industrial and medical purposes. Liquid oxygen is obtained from the oxygen found naturally in air by fractional distillation in a cryogenic air separation plant.

Air forces have long recognized the strategic importance of liquid oxygen, both as an oxidizer and as a supply of gaseous oxygen for breathing in hospitals and high-altitude aircraft flights. In 1985 the USAF started a program of building its own oxygen-generation facilities at all major consumption bases.[9][10]

In rocket propellant

{{see also|Liquid rocket propellant}}

Liquid oxygen is a common cryogenic liquid oxidizer propellant for spacecraft rocket applications, usually in combination with liquid hydrogen, kerosene or methane.[11][12]

Liquid oxygen was used in the very first liquid fueled rocket. The World War II V2 missile also used liquid oxygen under the name A-Stoff and Sauerstoff. In the 1950's, during the Cold War both the United States' Redstone and Atlas rockets, and the Soviet R-7 Semyorka used liquid oxygen. Later, in the 1960's & 70's, the ascent stages of the Apollo Saturn rockets, and the Space Shuttle main engines used liquid oxygen.

In 2018, many rockets use liquid oxygen:

  • Chinese space program: Long March 5, and its derivations Long March 6, Long March 7
  • Indian Space Research Organisation: GSLV
  • JAXA (Japan): H-IIA and H-IIB
  • Roscosmos (Russia): Soyuz-2 and Angara (under development)
  • ESA (EU): Ariane 5
  • USA
    • SpaceX: Falcon 9 and Falcon Heavy (at ~66 K, 10% denser than at boiling temperature)
    • United Launch Alliance: Atlas V, Delta IV Heavy, Vulcan (under development)
    • Northrop Grumman: Antares 230
    • Blue Origin: New Shepard and New Glenn (under development)
    • Rocket Lab: Electron

History

  • By 1845, Michael Faraday had managed to liquefy most gases then known to exist. Six gases, however, resisted every attempt at liquefaction[13] and were known at the time as "permanent gases". They were oxygen, hydrogen, nitrogen, carbon monoxide, methane, and nitric oxide.
  • In 1877, Louis Paul Cailletet in France and Raoul Pictet in Switzerland succeeded in producing the first droplets of liquid air.
  • The first measurable quantity of liquid oxygen was produced by Polish professors Zygmunt Wróblewski and Karol Olszewski (Jagiellonian University in Kraków) on April 5, 1883.

See also

{{Commons category|Liquid oxygen}}{{div col|colwidth=22em}}
  • Oxygen storage
  • Industrial gas
  • Cryogenics
  • Karol Olszewski and Zygmunt Florenty Wróblewski
  • Liquid hydrogen
  • Liquid helium
  • Liquid nitrogen
  • List of Stoffs
  • Natterer compressor
  • Rocket fuel
  • Solid oxygen
  • Tetraoxygen
{{div col end}}

References

1. ^{{Cite web|url=https://www.history.com/this-day-in-history/first-liquid-fueled-rocket|title=First liquid-fueled rocket|last=Editors|first=History com|website=HISTORY|language=en|access-date=2019-03-16}}
2. ^{{cite book|author1=Moore, John W. |author2=Stanitski, Conrad L. |author3=Jurs, Peter C. |title=Principles of Chemistry: The Molecular Science|url=https://books.google.com/books?id=ZOm8L9oCwLMC&pg=PA297|accessdate=3 April 2011|date=21 January 2009|publisher=Cengage Learning|isbn=978-0-495-39079-4|pages=297–}}
3. ^[https://web.archive.org/web/20080607160832/http://www.chemistry.ohio-state.edu/ehs/handbook/gases/cryosafe.htm Cryogenic Safety]. chemistry.ohio-state.edu.
4. ^Characteristics {{webarchive|url=https://web.archive.org/web/20120218125124/http://www.lindecanada.com/en/aboutboc/safety/cryogenic_liquids/characteristics.php |date=2012-02-18 }}. Lindecanada.com. Retrieved on 2012-07-22.
5. ^[[https://archive.org/details/23004LiquidOxygenReceiptTransferStorageDisposal Liquid Oxygen Receipt, Handling, Storage and Disposal - USAF Training Film }}
6. ^{{cite journal|last = Lewis|first = Gilbert N.|authorlink = Gilbert N. Lewis|year = 1924|title = The Magnetism of Oxygen and the Molecule O2|journal = Journal of the American Chemical Society|volume = 46|issue = 9|pages = 2027–2032|doi = 10.1021/ja01674a008}}
7. ^{{cite journal|last = Oda|first = Tatsuki|author2=Alfredo Pasquarello |year = 2004 |url=http://ir.library.tohoku.ac.jp/re/bitstream/10097/40070/1/e134402.pdf|title = Noncollinear magnetism in liquid oxygen: A first-principles molecular dynamics study|journal = Physical Review B|volume = 70|issue = 134402|pages = 1–19|doi = 10.1103/PhysRevB.70.134402|bibcode = 2004PhRvB..70m4402O }}
8. ^Cryo Techs: Providing the breath of life. af.mil (2014-09-05)
9. ^Arnold, Mark. 1U.S. Army Oxygen Generation System Development. RTO-MP-HFM-182. dtic.mil
10. ^{{cite book|url=https://books.google.com/books?id=LVfaBwAAQBAJ&pg=PA150|title=Advances in Cryogenic Engineering: Proceedings of the 1957 Cryogenic Engineering Conference, National Bureau of Standards Boulder, Colorado, August 19–21, 1957|author=Timmerhaus, K. D.|date=8 March 2013|publisher=Springer Science & Business Media|isbn=978-1-4684-3105-6|pages=150–}}
11. ^{{cite news |last=Belluscio|first=Alejandro G. |title=SpaceX advances drive for Mars rocket via Raptor power |url=http://www.nasaspaceflight.com/2014/03/spacex-advances-drive-mars-rocket-raptor-power/ |accessdate=March 13, 2014 |newspaper=NASAspaceflight.com |date=March 7, 2014 }}
12. ^{{cite news|last=Todd |first=David |title=Musk goes for methane-burning reusable rockets as step to colonise Mars |url=http://www.flightglobal.com/blogs/hyperbola/2012/11/musk-goes-for-methane-burning.html |accessdate=November 22, 2012 |newspaper=FlightGlobal Hyperbola |date=November 20, 2012 |quote=‘We are going to do methane,’ Musk announced as he described his future plans for reusable launch vehicles including those designed to take astronauts to Mars within 15 years, ‘The energy cost of methane is the lowest and it has a slight Isp (Specific Impulse) advantage over Kerosene’ said Musk adding, ‘and it does not have the pain in the ass factor that hydrogen has.’ ... SpaceX's initial plan will be to build a lox/methane rocket for a future upper stage codenamed Raptor. ... The new Raptor upper stage engine is likely to be only the first engine in a series of lox/methane engines. |deadurl=yes |archiveurl=https://web.archive.org/web/20121128070948/http://www.flightglobal.com/blogs/hyperbola/2012/11/musk-goes-for-methane-burning.html |archivedate=November 28, 2012 }}
13. ^Cryogenics. Scienceclarified.com. Retrieved on 2012-07-22.
{{DEFAULTSORT:Liquid Oxygen}}

6 : Rocket oxidizers|Cryogenics|Oxygen|Industrial gases|Liquids|1883 in science

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/11 1:10:14