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Nitrous oxide fuel blend

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155:. It is far less toxic than hydrazine and has a much lower boiling point, though it can be liquified at room temperature under pressure. Like hydrazine it has a positive enthalpy of formation that makes it both potentially unstable and a viable monopropellant. It can be decomposed with a catalyst to produce a hot mixture of nitrogen and oxygen. When mixed with a fuel and stored before use, it becomes a mixed monopropellant. 1414: 167:. The promise of high performance, greater range and lighter feed systems drove experimentation with blends of nitrous oxide and ammonia, which resulted in numerous explosions and demolished motors. The complexities involved in building propulsion systems that can safely handle nitrous oxide fuel blend monopropellants have been a deterrent to serious development. 716: 145:, can be used as a monopropellant to greatly simplify system design. But it is also extremely toxic and has a relatively high freezing point of +1C. It is also unstable, an inherent property of any substance with a positive enthalpy of formation. 189:(ISS), with an initial tentative flight date no earlier than 2012. NASA formally approved the mission to the ISS on a 2013 launch slot in May 2012. The mission had been slated to travel to the ISS in the unpressurized cargo compartment of a 193:
spacecraft during one of the contracted NASA cargo re-supply missions in mid-2013. The "ISPS NOFBX Green Propellant Demonstration" will utilize a deep-throttling 100 pounds-force (440 N)-thrust-class engine burning NOFBX
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contract. NOFBX was promoted by the company at the time as a "game changing" technology with the several characteristics that underline why safer monopropellants were of interest in the industry:
73:, cost, toxicity, risk of explosions, and other problems make it important for engineers to design rockets with appropriate propellants. The major classes of rocket fuels are: 695: 748: 1144: 1262: 369:
paper on the decomposition of nitrous oxide has raised concerns about the safety risks of mixing hydrocarbons with nitrous oxide. By adding hydrocarbons, the
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German rocket scientists were experimenting with nitrous oxide fuel blends as early as 1937. Nitrous oxide fuel blends testing continued throughout
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decomposes into oxygen-rich gasses. Combustion then ensues. Special care is needed in the chemical formulation and engine design to prevent
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on the ISS, and had been expected to remain on-orbit for approximately one year while undergoing a "series of in-space performance tests."
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blended mono-propellant developed by Firestar Technologies. The NOFBX patent claimed a mixture of nitrous oxide as the oxidizer with
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is a monopropellant, which significantly reduces the need for auxiliary hardware, saving cost, volume, and mass for launch systems
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is tolerant to a wide thermal range; storable at room temperature on the ground as well as in temperatures found in outer space
240:. Flight testing of NOFBX engines had been planned on the International Space Station, but, in the event, did not go forward. 1165: 1030: 734: 1269: 1124: 1093: 1088: 506: 532: 1438: 186: 474: 1224: 1083: 87: 25: 1443: 1257: 1016: 990: 932: 916: 906: 646:. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford, CT: Aerospace Research Central. 39:
In nitrous-oxide fuel blends, the fuel and oxidizer are blended and stored; this is sometimes referred to as a
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The propellant used in a rocket engine plays an important role in both engine design and in design of the
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Subsequent development of nitrous oxide fuel blends picked up again in the 2000s, and in 2011 an in-
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was projected to lower cost compared to existing propulsion systems of comparable performance
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constituents are widely available from chemical suppliers, inexpensive and safe to handle
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and produce no accumulated deposits or contamination; whereas hydrazine emits ammonia
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can be used as an oxidizer with various fuels; it is popular mainly in
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utilizes thrusters that run cooler, reducing thermal design challenges
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can be transported and handled without undue precautions or hazards
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mission was planned. In the event, the flight test was cancelled.
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Karabeyoglu, A. (2008). "Modeling of N2O Decomposition Events".
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to an explosive decomposition event is lowered significantly.
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and related ground equipment to service the vehicle. Weight,
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NOFBX was a trademarked name for a proprietary nitrous oxide/
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had announced plans to test the NOFBX mono-propellant on the
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that were intended in the early 2010s to be able to replace
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Ignition!: An Informal History of Liquid Rocket Propellants
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USPAT 20090133788 Nitrous oxide fuel blend monopropellants
696:"Green Propulsion Demo Passes Space Station Safety Review" 141:. It is liquid at room temperature and, having a positive 591:. Firestar Technologies. February 9, 2011. Archived from 533:"ISS-bound Propellant Demo Passes NASA Safety Review" 705:(talks about the (then upcoming) NASA safety review) 314:) are all substantially less toxic than traditional 1327: 1306: 1250: 1197: 1188: 1153: 1107: 1076: 1038: 1029: 999: 968: 925: 899: 892: 829: 764: 507:"SpaceX To Deliver Green-Propulsion Testbed To ISS" 330:of about 230 s; NOFBX was reported to have an 644:American Institute of Aeronautics and Astronautics 580: 578: 576: 505: 694:Doug Mohney (May 17, 2012). Brooke Neuman (ed.). 400: 398: 198:that will be mounted to the outside the European 423:(online publication date precedes print edition) 137:A common fuel in small maneuvering thrusters is 344:, more than three times greater than hydrazine 742: 247:to power high-altitude, long-endurance drone 8: 468: 466: 464: 462: 460: 458: 1194: 1035: 896: 749: 735: 727: 664:Sutton, George P.; Biblarz, Oscar (2001). 475:"A Non-Toxic Fuel From the Mojave Desert" 243:NOFBX had previously been used to fuel a 36:rocket propellent in some applications. 1161:Atmosphere-breathing electric propulsion 611: 609: 607: 605: 394: 316:long-duration storable monopropellants 7: 485:from the original on October 7, 2011 22:Nitrous oxide fuel blend propellants 504:Morring, Frank Jr. (May 21, 2012). 179:Innovative Space Propulsion Systems 1066:Field-emission electric propulsion 512:Aviation Week and Space Technology 16:Class of liquid rocket propellants 14: 1140:Microwave electrothermal thruster 1412: 473:Messier, Doug (August 9, 2011). 225:as the fuel. NOFBX has a higher 586:"NOFBX Monopropulsion Overview" 405:Joiner, Stephen (May 1, 2011). 108:Designs using one or more fuels 1270:Pulsed nuclear thermal rocket‎ 1166:High Power Electric Propulsion 1: 1125:Helicon double-layer thruster 1094:Electrodeless plasma thruster 1089:Magnetoplasmadynamic thruster 441:. Rutgers University Press. 411:Air & Space Smithsonian 187:International Space Station 1460: 666:Rocket Propulsion Elements 561:. Firestar-engineering.com 58: 1410: 1084:Pulsed inductive thruster 539:. May 29, 2012. p. 9 88:Liquid rocket propellants 26:liquid rocket propellants 1258:Nuclear pulse propulsion 1017:Electric-pump-fed engine 917:Hybrid-propellant rocket 907:Liquid-propellant rocket 717:NOFBX patent application 1314:Beam-powered propulsion 1287:Fission-fragment rocket 1242:Nuclear photonic rocket 1210:Nuclear electric rocket 976:Staged combustion cycle 912:Solid-propellant rocket 407:"The Mojave Launch Lab" 1365:Non-rocket spacelaunch 1215:Nuclear thermal rocket 1115:Pulsed plasma thruster 1031:Electrical propulsion 758:Spacecraft propulsion 670:John Wiley & Sons 143:enthalpy of formation 1263:Antimatter-catalyzed 1061:Hall-effect thruster 874:Solar thermal rocket 245:reciprocating engine 41:mixed monopropellant 1205:Direct Fusion Drive 1120:Vacuum arc thruster 1007:Pressure-fed engine 986:Gas-generator cycle 893:Chemical propulsion 830:Physical propulsion 652:10.2514/6.2008-4933 1439:Rocket propellants 1419:Spaceflight portal 1385:Reactionless drive 1350:Aerogravity assist 1190:Nuclear propulsion 265:its end products ( 1426: 1425: 1380:Atmospheric entry 1335:Orbital mechanics 1302: 1301: 1184: 1183: 1135:Resistojet rocket 1025: 1024: 1000:Intake mechanisms 933:Liquid propellant 837:Cold gas thruster 598:on July 24, 2011. 448:978-0-8135-0725-5 321:hydrazine has an 134: 133: 93:Solid propellants 61:Rocket propellant 51:the stored fuel. 1451: 1416: 1400:Alcubierre drive 1390:Field propulsion 1340:Orbital maneuver 1328:Related concepts 1195: 1046:Colloid thruster 1036: 897: 799:Specific impulse 751: 744: 737: 728: 706: 703: 683: 668:(7th ed.). 656: 655: 639: 633: 632: 630: 628: 613: 600: 599: 597: 590: 582: 571: 570: 568: 566: 555: 549: 548: 546: 544: 529: 523: 522: 520: 518: 509: 501: 495: 494: 492: 490: 470: 453: 452: 431: 425: 424: 421: 419: 417: 402: 313: 312: 311: 301: 300: 299: 289: 287: 286: 276: 275: 274: 227:specific impulse 77: 32:as the standard 1459: 1458: 1454: 1453: 1452: 1450: 1449: 1448: 1444:Monopropellants 1429: 1428: 1427: 1422: 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Index

liquid rocket propellants
hydrazine
storable
nitrous oxide
detonating
Rocket propellant
launch vehicle
energy density
Liquid rocket propellants
Solid propellants
Hybrid rocket
Monopropellants
Bipropellants
Tripropellants
hydrazine
enthalpy of formation
Nitrous oxide
hybrid rockets
World War II
space
flight test
Innovative Space Propulsion Systems
NASA
International Space Station
SpaceX Dragon
rocket engine
Columbus module
fuel
emulsifier
ethane

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