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High-test peroxide
View on WikipediaHigh-test peroxide (HTP) is a highly concentrated (85 to 98%) solution of hydrogen peroxide, with the remainder consisting predominantly of water. In contact with a catalyst, it decomposes into a high-temperature mixture of steam and oxygen, with no remaining liquid water. It was used as a propellant of HTP rockets and torpedoes, and has been used for high-performance vernier engines.
Properties
[edit]Hydrogen peroxide works best as a propellant in extremely high concentrations (roughly over 70%). Although any concentration of peroxide will generate some hot gas (oxygen plus some steam), at concentrations above approximately 67%, the heat of decomposing hydrogen peroxide becomes large enough to completely vaporize all the liquid at standard pressure. This represents a safety and utilization turning point, since decomposition of any concentration above this amount is capable of transforming the liquid entirely to heated gas (the higher the concentration, the hotter the resulting gas). This very hot steam/oxygen mixture can then be used to generate maximal thrust, power, or work, but it also makes explosive decomposition of the material far more hazardous.[1]
Normal propellant-grade concentrations, therefore, vary from 70 to 98%, with common grades of 70, 85, 90, and 98%.[2]
The volume change of peroxide due to freezing varies with percentage. Lower concentrations of peroxide (45% or less) will expand when frozen, while higher concentrations (65% or greater) will contract.[3]: 4–39
Hydrogen peroxide becomes more stable with higher peroxide content. For example, 98% hydrogen peroxide is more stable than 70% hydrogen peroxide. Water acts as a contaminant, and the higher the water concentration the less stable the peroxide is. The storability of peroxide is dependent on the surface-to-volume ratio of the materials the fluid is in contact with. To increase storability, the ratio should be minimized.[4]
Applications
[edit]When used with a suitable catalyst, HTP can be used as a monopropellant,[5] or with a separate fuel as a bipropellant.[6]
HTP has been used safely and successfully in many applications, beginning with German usage during World War II, and continues to the present day.[7] During World War II, high-test peroxide was used as an oxidizer in some German bipropellant rocket designs, such as the Walter HWK 509A rocket engine that powered the Messerschmitt Me 163 point defense interceptor fighter late in World War II, comprising 80% of the standardized mixture T-Stoff, and also in the German Type XVII submarine.
Some significant United States programs include the reaction control thrusters on the X-15 program, and the Bell Rocket Belt. The NASA Lunar Lander Research Vehicle used it for rocket thrust to simulate a lunar lander.
The Royal Navy experimented with HTP as the oxidiser in the experimental high-speed target/training submarines Explorer and Excalibur between 1958 and 1969.
The first Russian HTP torpedo was known by the strictly functional name of 53-57, the 53 referring to the diameter in centimeters of the torpedo tube, the 57 to the year it was introduced. Driven by the Cold War competition, they ordered the development of a larger HTP torpedo, to be fired from the 65-centimeter (26-inch) tubes. HTP in one of these Type 65 torpedoes on August 12, 2000 exploded on board and sank the K-141 Kursk submarine.
British experiments with HTP as a torpedo fuel were discontinued after a peroxide fire resulted in the loss of the submarine HMS Sidon (P259) in 1956.
British experimentation with HTP continued in rocketry research, ending with the Black Arrow launch vehicles in 1971. Black Arrow rockets successfully launched the Prospero X-3 satellite from Woomera, South Australia using HTP and kerosene fuel.
The British Blue Steel missile, attached to Vulcan and Victor bombers, in the 1960s, was produced by Avro. It used 85% concentration of HTP. To light the twin chamber Stentor rocket, HTP passed through a catalyst screen. Kerosene was then injected into the two chambers to produce 20,000 and 5,000 pounds (9,100 and 2,300 kilograms) of thrust each. The larger chamber was for climbing and accelerating, while the small chamber was to maintain cruise speed. The missile had a range of 100 nautical miles when launched at high altitude and about 50 nautical miles launched at low level (500 to 1,000 feet (150 to 300 metres)). Its speed was about Mach 2.0. After a high altitude launch it would climb to 70,000 to 80,000 feet (21,000 to 24,000 metres). From a low level launch, it would climb to only 40,000 feet (12,000 metres) but its speed would still be around Mach 2.0
With concentration of 82%, it is still in use on the Russian Soyuz rocket to drive the turbopumps on the boosters and on the orbital vehicle.
The Blue Flame rocket-powered vehicle achieved the world land speed record of 622.407 miles per hour (1,001.667 km/h) on October 23, 1970, using a combination of high-test peroxide and liquified natural gas (LNG), pressurized by helium gas.
Propellant-grade hydrogen peroxide is being used on current military systems and is in numerous defense and aerospace research and development programs. Many privately funded rocket companies are using hydrogen peroxide, such as Blue Origin and the defunct Armadillo Aerospace; and some amateur groups have expressed interest in manufacturing their own peroxide, both for their use and for sale in small quantities to others. HTP is used on ILR-33 AMBER[8] and Nucleus[9] suborbital rockets.
HTP was planned for use in an attempt to break the land speed record with the Bloodhound SSC car, aiming to reach over 1,000 miles per hour (1,600 km/h). HTP would have been the oxidiser for the hybrid fuel rocket, reacting with the solid fuel hydroxyl-terminated polybutadiene. The project stalled due to the Covid-19 pandemic and lack of funding.
Availability
[edit]This section needs additional citations for verification. (April 2025) |
Propellant-grade hydrogen peroxide is available to qualified buyers. In typical circumstances, this chemical is sold only to companies or government institutions that have the ability to properly handle and utilize the material. Non-professionals have purchased hydrogen peroxide of 70% or lower concentration (the remaining 30% is water with traces of impurities and stabilizing materials, such as tin salts, phosphates, nitrates, and other chemical additives), and increased its concentration themselves. Distillation is extremely dangerous with hydrogen peroxide; peroxide vapor can not ignite but the released oxygen can ignite any material that it is in contact with, detonation is possible depending on specific combinations of temperature and pressure, the detonation is the result of rapid reactive evaporation of the liquid resulting in high temperature and pressure resulting in a violent rupture of the containing vessel. In general, any boiling mass of high-concentration hydrogen peroxide at ambient pressure will produce vapor-phase hydrogen peroxide, which can detonate. This hazard is mitigated, but not eliminated, with vacuum distillation. Other approaches for concentrating hydrogen peroxide are sparging and fractional crystallization.
Hydrogen peroxide in concentrations of at least 35% appear on the US Department of Homeland Security's Chemicals of Interest list.[10]
Safety
[edit]Since many common substances catalyze peroxide's exothermic decomposition into steam and oxygen, handling of HTP requires special care and equipment. It is noted that the common materials iron and copper are incompatible with peroxide, but the reaction can be delayed for seconds or minutes, depending on the grade of peroxide used.
Small hydrogen peroxide spills are easily dealt with by flooding the area with water. Not only does this cool any reacting peroxide but it also dilutes it thoroughly. Therefore, sites that handle hydrogen peroxide are often equipped with emergency showers, and have hoses and people on safety duty.
Contact with skin causes immediate whitening due to the production of oxygen below the skin. Extensive burns occur unless washed off in seconds. Contact with eyes can cause blindness, and so eye protection is usually used.
The Kursk submarine disaster involved the accidental release of HTP in a torpedo which reacted with the torpedo's fuel.
References
[edit]- ^ "HYDROGEN PEROXIDE, STABILIZED | CAMEO Chemicals | NOAA". cameochemicals.noaa.gov. Retrieved 2025-12-29.
- ^ "MIL-PRF-16005F Performance Specification: Propellant, Hydrogen Peroxide" (PDF). Department of Defense Index of Specifications and Standards. 1 August 2003. Retrieved 12 November 2016 – via Whiskey Yankee LLC.
- ^ "Fire, Explosion, Compatibility and Safety Hazards of Hydrogen Peroxide" (PDF). NASA.
- ^ Ventura, Mark. Long Term Storability of Hydrogen Peroxide. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. General Kinetics Inc. AIAA-2005-4551.
- ^ "Green Hydrogen Peroxide (H2O2) Monopropellant with Advanced Catalyst Beds". ESA. Retrieved July 25, 2018.
- ^ "Development of a Low Thrust Bipropellant Thruster Based on Green Propellants". ESA. Retrieved July 25, 2018.
- ^ Ventura, M.; Garboden, G. (19 June 1999). "A Brief History of Concentrated Hydrogen Peroxide Uses" (PDF). General Kinetics. Retrieved 12 November 2016 – via Whiskey Yankee LLC.
- ^ Cieśliński, Dawid (2021). "Polish civil rockets' development overview".
- ^ "Nucleus: A Very Different Way to Launch into Space". Nammo. Retrieved 2022-02-06.
- ^ Department of Homeland Security (20 November 2007). "Appendix to Chemical Facility Anti-Terrorism Standards; Final Rule" (PDF). Federal Register. 72 (223): 65421–65435. Retrieved 12 November 2016.
High-test peroxide
View on GrokipediaChemical Properties
HTP exhibits strong oxidizing properties due to its high oxygen content—94% in 98% concentrations, with 46% usable oxygen—and decomposes exothermically into water and oxygen gas, releasing approximately 2.887 MJ/kg of energy at around 1267 K.[2] This decomposition is catalyzed by impurities, metals, or heat, making stability dependent on purity, pH (optimal near neutral), and temperature; pure solutions remain stable for over a year when stored at 8°C with stabilizers like sodium stannate.[1][3] Non-cryogenic and low-volatility, HTP offers high density and storability advantages over cryogenic oxidizers like liquid oxygen.[2]Applications in Propulsion
Primarily employed in rocketry since the 1940s, HTP serves as a monopropellant in thrusters for satellite attitude control, achieving specific impulses up to 180 seconds, and as an oxidizer in bipropellant or hybrid systems, enabling theoretical specific impulses of around 300 seconds in hybrid systems.[1][2] Historical uses include the Syncom satellite missions and modern hybrid rockets like the Polish ILR-33 AMBER, including its 2024 suborbital flight reaching space, and Nammo's Nucleus motor (2018 flight).[2][4] Its performance rivals ammonium perchlorate composites (305 s Isp) and matches hypergolic systems like nitrogen tetroxide/monomethylhydrazine, with added benefits from metal additives for enhanced thrust.[2]Advantages and Environmental Benefits
As a non-toxic, environmentally benign alternative to hydrazine-based propellants, HTP produces only water and oxygen upon decomposition, avoiding hazardous combustion byproducts like hydrochloric acid and reducing bioaccumulation risks.[2][1] It lowers handling costs, simplifies thruster designs due to its stability, and supports hypergolic ignition in combinations with fuels like kerosene, making it suitable for cost-efficient, eco-friendly aerospace applications.[1]Production, Safety, and Handling
HTP is produced via vacuum fractional distillation of lower-concentration solutions in specialized apparatus, yielding up to 99.9% purity in laboratory settings, with commercial production using industrial distillation processes.[1] Safety concerns arise from its reactivity: contamination with metals or organics can trigger violent decomposition, pressure buildup, or explosions, classifying 98% HTP as a potential Class 1 explosive; it also causes severe irritation or burns on skin/eye contact.[5][6] Proper handling requires inert materials (e.g., stainless steel or Teflon), stabilization, and controlled storage to mitigate risks, as evidenced by historical incidents involving storage and transportation.[7][8]Definition and History
Definition
High-test peroxide (HTP) is a highly concentrated aqueous solution of hydrogen peroxide (H₂O₂), typically containing 85% to 98% H₂O₂ by weight, with the balance primarily consisting of water.[9][2] This formulation distinguishes it from lower-concentration hydrogen peroxide solutions used in industrial or medical applications, as the elevated purity enables specialized uses requiring high reactivity and energy release.[10] A key characteristic of HTP is its high energy density, arising from the exothermic catalytic or thermal decomposition reaction:This process liberates significant heat, producing superheated steam and oxygen gas.[11] The designation "high-test" applies to concentrations above approximately 70% H₂O₂, at which point the solution exhibits effective monopropellant behavior, with the decomposition enthalpy sufficient to fully vaporize the reaction products.[12]
Historical Development
Hydrogen peroxide was first isolated in 1818 by French chemist Louis Jacques Thénard, who produced it by reacting barium peroxide with nitric acid, naming it "eau oxygénée" or oxygenated water. Early preparations yielded dilute solutions, limited by instability and decomposition, which restricted applications to low-concentration uses such as bleaching natural dyes and textiles in the 19th century.[13] In the 1920s and 1930s, German engineer Hellmuth Walter advanced research on concentrated hydrogen peroxide, developing it as a monopropellant for submarine propulsion and early rocket engines to enable closed-cycle operations without external air.[14] Walter's work focused on stabilizing high-strength solutions, known as T-Stoff (around 80-85% H₂O₂), which decomposed exothermically over catalysts to generate steam and oxygen for thrust.[15] This laid the groundwork for propulsion applications, culminating in the first powered flight of the Messerschmitt Me 163 Komet rocket interceptor on October 2, 1941, powered by a Walter HWK 109-509 engine using HTP as the primary oxidizer.[16] Following World War II, HTP saw adoption in several aerospace programs. The United States incorporated it into the X-15 hypersonic research aircraft's reaction control system during the 1950s and 1960s, where small thrusters decomposed 90% HTP for attitude control in near-space environments.[17] Britain utilized HTP/kerosene bipropellant engines in the Black Knight sounding rocket series starting in the mid-1950s, achieving multiple successful launches for re-entry vehicle testing.[18] The Soviet Union integrated HTP monopropellant thrusters into the Soyuz spacecraft's launch escape system and attitude control from the 1960s onward, relying on its reliability for crew safety and orbital maneuvers. The risks of HTP were dramatically illustrated in the 2000 Kursk submarine disaster, where a faulty weld in a Type 65 torpedo caused a hydrogen peroxide leak, leading to a chain of explosions that sank the vessel and killed all 118 crew members.[19] In the 2010s, HTP featured in the Bloodhound SSC project as the oxidizer in a hybrid rocket engine aimed at breaking the land speed record, highlighting its continued relevance in high-performance propulsion despite handling challenges.[20] In the 2020s, renewed interest in HTP as a "green" propellant led to several advancements. Benchmark Space Systems qualified a 22 N bipropellant hydrogen peroxide thruster in 2025, achieving flight heritage for small satellite propulsion.[21] Research also progressed on green bipropellant engines using 98% HTP as an oxidizer, with studies demonstrating improved performance and environmental benefits for spacecraft applications as of 2025.[22]Properties
Physical Properties
High-test peroxide (HTP), typically referring to aqueous hydrogen peroxide solutions with concentrations of 85% or higher by weight, exhibits physical properties that vary with concentration and temperature. These solutions are denser than water, with densities ranging from approximately 1.39 g/cm³ for 90% H₂O₂ to 1.43 g/cm³ for 98% H₂O₂ at 25°C.[23] As concentration increases toward 100% (anhydrous H₂O₂), the density reaches about 1.45 g/cm³ at 20°C, though practical HTP formulations rarely exceed 98% due to stability issues.[24] The boiling point of pure H₂O₂ is 150.2°C at standard atmospheric pressure, but concentrated solutions like HTP tend to decompose exothermically before reaching this temperature, releasing oxygen and water vapor.[24] For 90% and 98% solutions, extrapolated boiling points are approximately 141°C and 148°C, respectively, under 1 atm.[23] Vapor pressure increases with temperature, contributing to the handling challenges of these volatile liquids. Freezing points for HTP decrease initially with concentration but rise toward purity; 90% H₂O₂ freezes at -11.5°C, while 98% freezes at -2.5°C, and pure H₂O₂ at -0.43°C.[23][24] Unlike dilute aqueous solutions that expand upon freezing like water, high-concentration HTP (>90%) contracts, as the density of anhydrous H₂O₂ increases from ~1.46 g/cm³ (liquid at 0°C) to 1.64–1.71 g/cm³ (solid at -20°C).[24][25] Viscosity of HTP is higher than that of water (0.89 mPa·s at 20°C), with values around 1.15 mPa·s for 90% H₂O₂ at 25°C and 1.24 mPa·s for pure H₂O₂ at 20°C, which influences flow behavior.[23][24] Surface tension is also elevated, at approximately 80 mN/m for concentrations near 100% at 20°C compared to water's 72 mN/m.[24] Optically, HTP is a clear, colorless liquid with a refractive index of about 1.40, ranging from 1.398 for 90% to 1.405 for 98% at 25°C.[23]| Property | 90% H₂O₂ (20-25°C) | 98% H₂O₂ (20-25°C) | Pure H₂O₂ (20-25°C) | Source |
|---|---|---|---|---|
| Density (g/cm³) | 1.39 | 1.43 | 1.45 | DTIC AD0268379, DTIC AD0022243 |
| Viscosity (mPa·s) | 1.15 | ~1.24 | 1.24 | DTIC AD0268379, DTIC AD0022243 |
| Surface Tension (mN/m) | ~80 | ~80 | 80.4 | DTIC AD0022243 |
| Refractive Index | 1.398 | 1.405 | 1.407 | DTIC AD0268379, DTIC AD0022243 |
