Editing Monopropellant

{{Short description|Single-part rocket propellant}}
'''Monopropellants'''<ref>{{Cite book
  |quote=A rocket propellant consisting of a single substance, especially a liquid, capable of creating rocket thrust without the addition of a second substance.
  |author=Sybil P. Parker
  |title=McGraw-Hill dictionary of scientific and technical terms
  |edition=6
  |year=2003
  |publisher=McGraw-Hill
  |isbn=978-0-07-042313-8
  |page=1370}}</ref> are [[propellants]] consisting of chemicals that release energy through exothermic chemical decomposition. The molecular bond energy of the monopropellant is released usually through use of a catalyst. This can be contrasted with bipropellants that release energy through the chemical reaction between an oxidizer and a fuel. While stable under defined storage conditions, monopropellants decompose very rapidly under certain other conditions to produce a large volume of its own energetic (hot) gases for the performance of mechanical [[work (physics)|work]]. Although solid [[Wikt:deflagrant|deflagrant]]s such as [[nitrocellulose]], the most commonly used propellant in firearms, could be thought of as monopropellants, the term is usually reserved for liquids in engineering literature.<ref>{{Cite book|last=Vere|first=Ray|url=https://books.google.com/books?id=YlhdDwAAQBAJ&pg=PA223|title=Aviation Fuels Technology|publisher=Macmillan Education UK|year=1985|isbn=978-1-349-06904-0|page=223}}</ref>

==Uses==
The most common use of monopropellants<ref name="spacehandbookprops">{{cite tech report|title=Space handbook: astronautics and its applications |chapter=Propellants |pages=42-46 |url=http://www.hq.nasa.gov/pao/History/conghand/propelnt.htm |last=RAND Corporation |editor1-last=Horgan |editor1-first=M. J. |editor2-last=Palmatier |editor2-first=M. A. |editor3-last=Vogel |editor3-first=J. |number=86 |publisher=United States Government Printing Office |date=1959}}</ref> is in low-impulse [[monopropellant rocket|monopropellant]] [[rocket motor]]s,<ref>{{cite web|url=http://www.rocketmotorparts.com/resources.html|archive-url=https://web.archive.org/web/20120114162923/http://www.rocketmotorparts.com/resources.html|archive-date=January 14, 2012|title=Resources|publisher=Rocket Motor Components, Inc.}}</ref> such as [[reaction control system|reaction control thrusters]], the usual propellant being [[hydrazine]]<ref>[http://www.aerojet.com/capabilities/spacecraft.php] {{webarchive|url=https://web.archive.org/web/20090928054803/http://www.aerojet.com/capabilities/spacecraft.php|date=September 28, 2009}}</ref><ref name="Sutton, 230" >{{harvnb|Sutton|1992}}, p.&nbsp;230</ref> which is generally decomposed by exposure to an [[iridium]]<ref>{{cite web |url=http://www.rocket.com/Aerojet%20Bipropellant%20Engine%20Sets%20New%20Performance%20Record |title=Aerojet Bipropellant Engine Sets New Performance Record |publisher=Aerojet Rocketdyne |date=December 8, 2008 |access-date=July 13, 2014 |archive-date=March 7, 2017 |archive-url=https://web.archive.org/web/20170307024506/http://www.rocket.com/Aerojet%20Bipropellant%20Engine%20Sets%20New%20Performance%20Record  }}</ref><ref name="Sutton, 307-309" >{{harvnb|Sutton|1992}}, pp.&nbsp;307—309</ref> [[catalyst]] bed (the hydrazine is pre-heated to keep the reactant liquid).  This decomposition produces the desired jet of hot gas and thus [[thrust]]. [[High-test peroxide|Hydrogen peroxide]]<ref name="spacehandbookpropuls">{{cite tech report|title=Space handbook: astronautics and its applications |chapter=Propulsion systems |pages=31-41 |url=http://www.hq.nasa.gov/pao/History/conghand/propulsn.htm |last=RAND Corporation |editor1-last=Horgan |editor1-first=M. J. |editor2-last=Palmatier |editor2-first=M. A. |editor3-last=Vogel |editor3-first=J. |number=86 |publisher=United States Government Printing Office |date=1959}}</ref> has been used as a power source for propellant tank pumps in rockets like the German WWII [[V-2 rocket|V-2]] and the American [[Redstone (rocket)|Redstone]].<ref>{{harvnb|Sutton|1992}}, ch. 7.</ref> The [[hydrogen peroxide]] is passed through a [[platinum]] [[catalyst]] mesh,<ref name="spacehandbookpropuls"/> or comes in contact with [[manganese dioxide]] impregnated ceramic beads, or [[Z-Stoff]] [[permanganate]] solution is co-injected,  which causes hydrogen peroxide to decompose into hot steam and oxygen.

Monopropellants are also used in some [[air-independent propulsion]] systems (AIP) to "fuel" reciprocating or [[turbine]] engines in environments where free oxygen is unavailable. Weapons intended primarily for combat between nuclear-powered [[submarines]] generally fall into this category. The most commonly used propellant in this case is stabilized [[propylene glycol dinitrate]] ([[PGDN]]), often referred to as "[[Otto Fuel II|Otto fuel]]".  A potential future use for monopropellants not directly related to propulsion is in compact, high-intensity powerplants for aquatic or exoatmospheric environments.

==Research in brief ==
Much work was done in the US in the 1950s and 1960s to attempt to find better and more energetic monopropellants. For the most part, researchers came to the conclusion that any single substance that contained enough energy to compete with bipropellants would be too unstable to handle safely under practical conditions. With new materials, control systems and requirements for high-performance thrusters, engineers are currently{{When|date=March 2011}} re-examining this assumption.{{Citation needed|date=March 2011}}

Many partially nitrated alcohol esters are suitable for use as monopropellants. "Trimethylene glycol dinitrate" <!-- a glycol must have the hydroxyls on adjacent carbon atoms --> or [[1,3-propanediol]] dinitrate is [[isomer]]ic with [[PGDN]], and produced as a fractional byproduct in all but the most exacting laboratory conditions; the marginally lower [[specific gravity]] (and thus [[energy density]]) of this compound argues against its use, but the minor differences in chemistry may prove useful in the future.{{Citation needed|date=March 2011}}

The related "dinitrodiglycol", more properly termed [[diethylene glycol dinitrate]] in modern notation, was widely used in World War 2 Germany, both alone as a liquid monopropellant and [[colloidal]] with [[nitrocellulose]] as a solid propellant. The otherwise desirable characteristics of this compound; it is quite stable, easy to manufacture, and has a very high energy density; are marred by a high [[freeze point]] (-11.5 deg. C) and pronounced thermal expansion, both being problematic in spacecraft. "Dinitrochlorohydrin" and "tetranitrodiglycerin" are also likely candidates, though no current use is known. The polynitrates of long chain and [[aromatic hydrocarbons]] are invariably room temperature solids, but many are soluble in simple alcohols or ethers in high proportion, and may be useful in this state.{{Citation needed|date=March 2011}}

[[Hydrazine]],<ref name="Sutton, 230" /><ref>{{cite web|url=http://cs.astrium.eads.net/sp/SpacecraftPropulsion/MonopropellantThrusters.html|archive-url=https://web.archive.org/web/20100327105117/http://cs.astrium.eads.net/sp/SpacecraftPropulsion/MonopropellantThrusters.html|archive-date=March 27, 2010|title=Monopropellant Hydrazine Thrusters|publisher=EADS Astrium}}</ref> [[ethylene oxide]],<ref>{{cite web|url=http://www.rocketmotorparts.com/resources/ethylene_oxide.pdf|archive-url=https://web.archive.org/web/20120321015445/http://www.rocketmotorparts.com/resources/ethylene_oxide.pdf|archive-date=March 21, 2012|title=ethylene_oxide.pdf}}</ref> [[hydrogen peroxide]] (especially in its German World War II form as ''[[T-Stoff]]''),<ref>{{cite web|url=http://www.rocketmotorparts.com/resources/h2o2.pdf|archive-url=https://web.archive.org/web/20120321015449/http://www.rocketmotorparts.com/resources/h2o2.pdf|archive-date=March 21, 2012|title=h2o2.pdf}}</ref> and [[nitromethane]]<ref>{{cite web|url=http://www.rocketmotorparts.com/resources/nitromethane.pdf|archive-url=https://web.archive.org/web/20120321015452/http://www.rocketmotorparts.com/resources/nitromethane.pdf|archive-date=March 21, 2012|title=nitromethane.pdf}}</ref> are common rocket monopropellants. As noted the specific impulse of monopropellants is lower<ref name="spacehandbookprops"/><ref>{{harvnb|Sutton|1992}}, p.&nbsp;36</ref> than bipropellants and can be found with the Air Force Chemical Equilibrium Specific Impulse Code tool.<ref>{{cite web|url=http://www.dunnspace.com/isp.htm|archive-url=https://web.archive.org/web/20131020061623/http://www.dunnspace.com/isp.htm|archive-date=October 20, 2013|title=Rocket Engine Specific Impulse Program|last=Dunn|first=Bruce P.|date=2001|publisher=Dunn Engineering}}</ref>

One newer monopropellant under development is [[nitrous oxide]], both neat and in the form of [[nitrous oxide fuel blend]]s.  Nitrous oxide offers the advantages of being self-pressurizing and of being relatively non-toxic, with a specific impulse intermediate between hydrogen peroxide and hydrazine.<ref name="ZakirovSweeting2001">{{cite journal|last1=Zakirov|first1=Vadim|last2=Sweeting|first2=Martin|last3=Lawrence|first3=Timothy|last4=Sellers|first4=Jerry|title=Nitrous oxide as a rocket propellant|journal=Acta Astronautica|volume=48|issue=5–12|year=2001|pages=353–362|doi=10.1016/S0094-5765(01)00047-9|bibcode=2001AcAau..48..353Z}}</ref> [[Nitrous oxide]] generates oxygen upon decomposition, and it is possible to blend it with fuels to form a monopropellant mixture with a specific impulse up to 325&nbsp;s, comparable to [[Hypergolic propellant|hypergolic bipropellants]].<ref name=awst20120521>{{cite news |last=Morring |first=Frank Jr. |title=SpaceX To Deliver Green-Propulsion Testbed To ISS |url=http://aviationweek.com/awin/spacex-deliver-green-propulsion-testbed-iss |access-date=July 13, 2014 |newspaper=Aviation Week and Space Technology |date=May 21, 2012}}</ref> In 2018 a new precious metal catalyst was invented for use with nitrous oxide -  rhodium oxide on alumina spheres – which is more stable at higher temperatures than pure rhodium or iridium.<ref>{{Cite web |title=Catalysts |url=https://www.americanelements.com/catalysts |access-date=2024-01-05 |website=American Elements |language=en}}</ref> 

Direct comparison of physical properties, performance, cost, storability, toxicity, storage requirements and accidental release measures for hydrogen peroxide, [[hydroxylammonium nitrate]] (HAN), hydrazine and various cold gas monopropellants shows that hydrazine is the highest performing in terms of specific impulse. However, hydrazine is also the most expensive and toxic. In addition HAN and hydrogen peroxide have the highest density impulse (total impulse per given unit volume).<ref name=Wernimont2006>{{cite journal|last1=Wernimont|first1=Eric|title=System Trade Parameter Comparison of Monopropellants: Hydrogen Peroxide vs Hydrazine and Others|journal=42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit|year=2006|doi=10.2514/6.2006-5236|isbn=978-1-62410-038-3|url=http://www.hydrogen-peroxide.us/chemical-handling-toxicity/AIAA-2006-5236_hydrogen_peroxide_versus_hydrazine.pdf}}</ref>

==See also==
*[[Monopropellant rocket]]
*[[Nitrous oxide fuel blend]]
*[[Green Propellant Infusion Mission]]

==References==
{{Reflist|30em}}

== Further reading ==
*{{Cite book
|last=Sutton  |first=George P.
|title=Rocket Propulsion Elements
|publisher=John Wiley & Sons  |location=New York
|orig-date=1949
|edition=6th
|year=1992
|isbn=0-471-52938-9
}}
* There is an entire chapter on the history of monopropellant development in the autobiography by {{cite book |isbn = 978-0-8135-9918-2 |title = Ignition!: An Informal History of Liquid Rocket Propellants |last1 = Clark |first1 = John Drury |author-link=John Drury Clark |date = 23 May 2018 |publisher = Rutgers University Press |url=https://books.google.com/books?id=BdU4DwAAQBAJ&q=monopropellant  |pages=302 |oclc=281664}}
* The book "Germany's Secret Weapons In World War Two" by Roger Ford ({{ISBN|0-7603-0847-0}} c.2000) contains some useful information on the surprising diversity of fuels and propellants employed by wartime Germany.
* "[[The Chemistry Of Powder And Explosives]]" by [[Tenney L. Davis]] is an outstanding, if outdated, source of  information on a great many aspects of high enthalpy compounds. (This work originally published by MIT Press, 1943, as a textbook. Subsidy republication as late as 1995 by Pyrotek Inc., an amateur rocketry supply house. No catalog data given in this edition. Current publication status unknown.).
* [http://www.hydrogen-peroxide.us/uses-monoprop-steam-generation/H2O2_Conf_1999-Past_Present_Uses_of_Rocket_Grade_Hydrogen_Peroxide.pdf 1999 Conference Paper on Historical Rocket Grade Hydrogen Peroxide Uses including monopropellant applications]
*{{Cite book |last=Schmidt |first=Eckart W. |title=Encyclopedia of Monopropellants |date=2023 |publisher=De Gruyter |isbn=978-3-11-075127-7 |edition=1st |location=Berlin/Boston |lccn=2023930404}}
*{{Cite journal |last=Nosseir |first=Ahmed E. S. |last2=Cervone |first2=Angelo |last3=Pasini |first3=Angelo |date=15 January 2021 |title=Review of State-of-the-Art Green Monopropellants: For Propulsion Systems Analysts and Designers |url=https://www.mdpi.com/2226-4310/8/1/20 |journal=Aerospace |volume=8 |issue=1 |article-number=20 |doi=10.3390/aerospace8010020 |issn=2226-4310 |doi-access=free|hdl=11572/393891 |hdl-access=free }}
==External links==
{{Commons category|Monopropellants}}


[[Category:Rocket propellants]]
[[Category:Monopropellants| ]]