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Supplier: Accuris
Description: Tracked Changes (Redline) - Explosives for civil uses - Propellants and rocket propellants - Part 5: Verification of safe functioning of solid rocket propellants used in small rocket motors
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Supplier: Accuris
Description: Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
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Supplier: Accuris
Description: Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
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Supplier: Accuris
Description: Explosives for civil uses Propellants and rocket propellants Part 1: Requirements
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Supplier: ASTM International
Description: 1.1 These definitions cover the flow properties of gelled propellants of interest to the aerospace industry.
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Supplier: SAE International
Description: This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.
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Supplier: ASTM International
Description: 1.1 This test method covers the measurement of solid propellant specific impulse values. 1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.
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Supplier: ASTM International
Description: liquid rocket propellants to hazard levels such that the use of quantity-distance criteria is not essential to assure public safety. 1.3 Application-The requirements of this guide shall apply to persons directly involved in the storage, use, or handling of liquid rocket
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Description: The great engineering achievement required to overcome most of the challenges and obstacles that prevented turning rocket design from art into science took place in Europe and the United States between the 1930s and the 1950s. With the vast majority of the engines currently in operation
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Supplier: SAE International
Description: Increased emphasis on rocket engine reliability and cost has prompted the Liquid Rocket Certification Subcommittee (Society of Automotive Engineers for Reliability, Maintainability, and Supportability) to thoroughly examine current methodologies to qualify or certify liquid
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Supplier: CSA Group
Description: ISO 16694:2015 applies to all types of liquid rocket engines for expendable launch systems and satellites: a) Combustible fuel (including cryogenic); b) Large-thrust, multiple component engines, with and without afterburning; c) Low-thrust engines, one component (mono-propellant) and
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Supplier: AENOR
Description: Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
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Supplier: AENOR
Description: Explosives for civil uses - Propellants and rocket propellants - Part 5: Verification of safe functioning of solid rocket propellants used in small rocket motors (Endorsed by Asociación Española de Normalización in January of 2026.)
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Supplier: AENOR
Description: Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
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Supplier: AENOR
Description: Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder
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Description: Reduce fire dangers and related hazards associated with high power rocketry using the latest safety guidelines in the 2018 edition of NFPA 1127. NFPA 1127: Code for High Power Rocketry applies to the design, construction, limitation of propellant mass and power, and reliability of high power
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Description: software. This edition allows another option for calculating the minimum launch site dimensions for original rocket designs or rocket kits, which cannot normally be obtained by manufacturers. This change permits a consumer to accurately calculate the altitude that any rocket
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GENERAL PLASTICS’ POLYURETHANE FOAM FILLS KEY ROLE IN GROUND TEST OF WORLD’S LARGEST SOLID ROCKET MOTOR (read more)
Browse Foams and Foam Materials Datasheets for General Plastics Manufacturing Co. -
used in modern industry. Rocket propellants, cryogenic fuels, and pressurized gases require rigorous monitoring from storage through launch. Hydrogen, for example, is highly flammable and difficult to detect (read more)
Browse Gas Sensors Datasheets for DOD Technologies Inc. -
Now more than ever it is important to monitor and control it's output. Nitrous oxide (N2O) is also known as “laughing gas”. It is not just used in medicine. It is also used in the food industry as a propellant for spray whipped cream (E 942), in (read more)
Browse Gas Sensors Datasheets for Electro Optical Components, Inc.
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Metal 3D Printing and Machining Produce High-Efficiency Rocket Designed by Stanford Students
. The organization supports a variety initiatives that range from biology and high-altitude balloons to satellites and rocketry. One group of students is heading up a project solely dedicated to creating a liquid propellant rocket with the goal of setting the world record for altitude reached
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Ampac's New Agenda
that developed missile and rocket propellants in work dating back to the 1940s and 1950s, explains Paul Kane, CFO and director of information systems. In the 1990s, Aerojet began to move into pharmaceutical manufacturing, in part to commercialize investments at the site. Eight years ago
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Zirconium in Hydrogen Peroxide Applications (.pdf)
agent for pulp and paper; and as an additive for treating solid, liquid and gaseous wastes. High Test Purity (HTP) hydrogen peroxide is also used as a fuel or propellant for rockets.
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SPACE | CRYOGENIC FLUID SAFE-SHEAR TM BURST DISCS
fluids is critical. An overpressure event could result in the catastrophic loss of a spacecraft. Another problem to consider is "Boil-off," the term given to the product losses from cryogenic propellant storage systems during long-duration space mission applications. Space-based applications of burst
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Rocketing Into the Future
250 Rocket propelled lifting bodies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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History of Liquid Propellant Rocket Engines > Liquid Propellant Rocket Engines in the United States (Summary)
These boron hydrides had been identified as a promising high-energy rocket propel- lants , rich in hydrogen content, with a specific impulse close to the theoretical value of over 350 s.
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Rocket and Spacecraft Propulsion
These came into use as gun propellants, after gunpowder, and it was natural that they should be considered as rocket propellants .
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Federal Register > Friday, August 11, 2006 > [71 FR 46079] Commerce in Explosives-Hobby Rocket Motors (2004R-7P)
… upon the statutory definition of "explosives," which contemplates that items can "function by explosion" either by detonating (dynamite and other high explosives detonate) or by deflagrating (low explosives, such as black powder, pellet powder, and rocket propellants , deflagrate, or burn very …
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Blazing the Trail: The Early History of Spacecraft and Rocketry
The gunpowder rocket propellant was modified to achieve lower burning rates and, correspondingly, less pressure in rocket casings.
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History of Liquid Propellant Rocket Engines > Liquid Propellant Rocket Engines in Russia, Ukraine, and the former Soviet Union
Sergei P. Korolev, an engineer and pilot, became the leader of the Moscow GIRD in 1932.2 ~4 He personally also worked on several vertically launched rocket test vehicles and rocket propelled aircraft.
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History of Liquid Propellant Rocket Engines > Technology and Hardware
The liquid rocket propellants are the working fluids of LPREs.
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Powered Flight
Looking at a solid rocket propellant ’s burning rate under pressure and core flow.
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Aerospace Propulsion Systems
NG = nitroglycerine NGV = nozzle guide vanes NOX = nitrous oxides OPR = overall (total) pressure ratio PSFC = power specific fuel consumption RAF = Royal Air Force ( UK ) RP = rocket propellant rpm = rotations per minute (rot/min) rps = rotations per second (rot/s) SC = single crystal SFC = specific …
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Rocket and Spacecraft Propulsion
These came into use as gun propellants after gunpowder, and it was natural that they should be considered as rocket propellants .