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propellant

propellant, Total:500 items.

In the international standard classification, propellant involves: Space systems and operations, Products of the chemical industry, Aircraft and space vehicles in general, Materials for aerospace construction, On-board equipment and instruments, Air quality, Aerospace engines and propulsion systems, Electricity. Magnetism. Electrical and magnetic measurements, Sports equipment and facilities, Internal combustion engines, Aerospace fluid systems and components, Fuels.

U.S. Military Regulations and Norms, propellant

• ARMY MIL-I-60016 A VALID NOTICE 3-2013 Increments, Propellant for Charge, Propelling, M36A1 (Made from Propellant, M8)
• ARMY MIL-I-60016 A NOTICE 2-1996 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A1 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-60016 A VALID NOTICE 1-1991 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A1 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-60016 A (5)-1982 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A1 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-60016 A-1969 MILITARY SPECIFICATION INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A1 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-48086 (4)-1990 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A2 (MADE FROM PROPELLANT M8)
• ARMY MIL-I-48086-1972 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A2 (MADE FROM PROPELLANT M8)
• ARMY MIL-I-48086 NOTICE 1-1997 INCREMENTS, PROPELLANT FOR CHARGE, PROPELLING, M36A2 (MADE FROM PROPELLANT M8)
• ARMY MIL-P-23929 A NOTICE 2-2013 PROPELLANT, H8
• ARMY MIL-I-3848 A NOTICE 1-1997 INDICATOR, PROPELLANT TEMPERATURE, M13, M15 AND M33 (LESS PROPELLANT)
• ARMY MIL-I-3848 A-1963 INDICATOR, PROPELLANT TEMPERATURE, M13, M15 AND M33 (LESS PROPELLANT)
• ARMY MIL-I-14961 REINST NOTICE 3-1996 INCREMENTS, PROPELLANT M1A1, M2A1, M3A1, M181 AND M182 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-14961 (4)-1992 INCREMENTS, PROPELLANT M1A1, M2A1, M3A1, M181 AND M182 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-14961 VALID NOTICE 1-1988 INCREMENTS, PROPELLANT M1A1, M2A1, M3A1, M181 AND M182 (MADE FROM PROPELLANT, M8)
• ARMY MIL-I-14961-1969 INCREMENTS, PROPELLANT M1A1, M2A1, M3A1, M181 AND M182 (MADE FROM PROPELLANT, M8)
• ARMY A-A-59402 VALID NOTICE 1-2003 DRUM (FOR BULK PROPELLANT)
• ARMY A-A-59402-1999 DRUM (FOR BULK PROPELLANT)
• ARMY MIL-P-50472 A VALID NOTICE 3-2013 Propellant M26A1, For Use in Change Propelling M189
• ARMY MIL-P-323 A NOTICE 1-1996 PROPELLANT, M2 AND M5
• ARMY MIL-P-323 A-1959 PROPELLANT, M2 AND M5
• ARMY A-A-59402 VALID NOTICE 2-2013 Drum (for Bulk Propellant)
• ARMY MIL-V-45120-1958 VALVE ASSEMBLY, PROPELLANT FILLER
• ARMY MIL-P-3984 J VALID NOTICE 1-2013 Propellants for Small Arms Ammunition
• ARMY MIL-P-63404 VALID NOTICE 2-2013 Propellant M6 For Use In Charge, Propelling, 155MM, M119A2
• ARMY MIL-P-48349 NOTICE 2-2013 PROPELLANT M30A1 FOR USE IN 155MM PROPELLING CHARGES
• ARMY MIL-S-48380 NOTICE 2-1996 SUPPORT, PROPELLING CHARGE (FOR USE IN AMMUNITION PACKING)
• ARMY MIL-S-48380 VALID NOTICE 1-1987 SUPPORT, PROPELLING CHARGE (FOR USE IN AMMUNITION PACKING)
• ARMY MIL-S-48380-1975 SUPPORT, PROPELLING CHARGE (FOR USE IN AMMUNITION PACKING)
• ARMY MIL-P-63194 A VALID NOTICE 3-2013 Propellant, M10 for 60MM Mortar M204 Propelling Charge
• ARMY MIL-P-60045 A VALID NOTICE 2-2013 Propellant M2 For Use In 165MM Cartridges
• ARMY MIL-P-60398 B NOTICE 1-2013 PROPELLANT M9, FLAKE (FOR USE IN IGNITION CARRTRIDGES)
• ARMY MIL-C-13609 B REINST NOTICE 3-1996 CASTING SOLVENT FOR OIA, OGK AND AHH PROPELLANTS
• ARMY MIL-C-13609 B VALID NOTICE 1-1988 CASTING SOLVENT FOR OIA, OGK AND AHH PROPELLANTS
• ARMY MIL-C-13609 B-1974 CASTING SOLVENT FOR OIA, OGK AND AHH PROPELLANTS
• ARMY MIL-H-48085 A NOTICE 2-1996 HOLDER, PROPELLANT FOR 4.2 INCH AMMUNITION
• ARMY MIL-H-48085 A VALID NOTICE 1-1987 HOLDER, PROPELLANT FOR 4.2 INCH AMMUNITION
• ARMY MIL-H-48085 A-1981 HOLDER, PROPELLANT FOR 4.2 INCH AMMUNITION
• ARMY MIL-P-60398 B-1988 PROPELLANT M9 FLAKE, FOR USE IN IGNITION CARTRIDGES
• ARMY MIL-T-45119-1958 TANK, LIQUID PROPELLANT, GUIDED MISSILE, M2
• ARMY MIL-P-60989 A VALID NOTICE 1-1988 PROPELLANT, M2 FOR M5 SUBSYSTEM AMMUNITION
• ARMY MIL-P-60989 A (1)-1980 PROPELLANT, M2 FOR M5 SUBSYSTEM AMMUNITION
• ARMY MIL-P-60989 A-1976 PROPELLANT, M2 FOR M5 SUBSYSTEM AMMUNITION
• ARMY MIL-STD-286 C CHG NOTICE 2-2010 PROPELLANTS, SOLID: SAMPLING, EXAMINATION AND TESTING
• ARMY MIL-DTL-60318 C (4)-2011 PROPELLANT, M1 FOR USE IN CHARGE, PROPELLING, M67 FOR 105MM HOWITZER
• ARMY MIL-C-60459 NOTICE 1-1996 CARTRIDGE, 105MM, HE, ROCKET ASSISTED, XM548, ROCKET PROPELLANT GRAIN FOR
• ARMY MIL-C-60459-1967 CARTRIDGE, 105MM, HE, ROCKET ASSISTED, XM548, ROCKET PROPELLANT GRAIN FOR
• ARMY MIL-P-50206 VALID NOTICE 1-1988 PROPELLANT M9, FLAKE (FOR USE IN 40MM CARTRIDGES)
• ARMY MIL-STD-652 D NOTICE 6-1990 PROPELLANTS, SOLID FOR CANNONS REQUIREMENTS AND PACKING
• ARMY MIL-P-63195 A NOTICE 1-2013 PROPELLANT M9 FOR USE IN CARTRIDGE, IGNITION M702
• ARMY MIL-P-48130 A NOTICE 2-2013 PROPELLANT M10 FOR 81MM MORTAR M205 PROPELLING CHARGE
• ARMY MIL-STD-1166 A NOTICE 1-2001 RADIOGRAPHIC TESTING REQUIREMENTS FOR SOLID PROPELLANTS
• ARMY MIL-STD-1166 A-1991 RADIOGRAPHIC TESTING REQUIREMENTS FOR SOLID PROPELLANTS
• ARMY MIL-STD-1171 A VALID NOTICE 3-2013 Acceptance and Description Sheets (for Propellants and Explosives)
• ARMY MIL-P-50206 (5)-2008 PROPELLANT M9, FLAKE (FOR USE IN 40MM CARTRIDGES)
• ARMY MIL-P-70533 VALID NOTICE 2-2013 Projectile, 105mm, HE, RA XM913/XM927 Rocket Propellant For
• ARMY MIL-P-50206 (4)-1998 PROPELLANT M9, FLAKE (FOR USE IN 40MM CARTRIDGES)
• ARMY MIL-P-50206-1968 PROPELLANT M9, FLAKE (FOR USE IN 40MM CARTRIDGES)
• ARMY MIL-STD-652 D NOTICE 7-2013 Propellants, Solid, for Cannons Requirements and Packing
• ARMY MIL-P-50202 A (7)-1998 PROPELLANT CHARGE, ROCKET, FOR DEMOLITION KIT, CRATERING, M180
• ARMY MIL-P-50202 A-1977 PROPELLANT CHARGE, ROCKET, FOR DEMOLITION KIT, CRATERING, M180
• ARMY MIL-H-45704-1959 HOSE ASSEMBLY, PROPELLANT TRANSFER, OXIDIZER AND FUEL
• ARMY MIL-P-63194 A NOTICE 2-1996 PROPELLANT, M10 FOR 60MM MORTAR M204 PROPELLING CHARGE
• ARMY MIL-P-63203 NOTICE 1-1996 PROJECTILE, 155MM, HE, RA, M549A1 AFT (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-63105 B VALID NOTICE 3-2013 Propellant M30 for use in Cartridge 105MM, APFSDS-T, M735, M735A1, and XM774
• ARMY MIL-P-70533 (6)-1998 PROJECTILE, 105MM, HE, RA, XM913/XM927 ROCKET PROPELLANT FOR
• ARMY MIL-P-70533 NOTICE 1-1998 PROJECTILE, 105MM, HE, RA, XM913/XM927 ROCKET PROPELLANT FOR
• ARMY MIL-P-70533-1990 PROJECTILE, 105MM, HE, RA, XM913/XM927 ROCKET PROPELLANT FOR
• ARMY MIL-P-63203 (2)-1987 PROJECTILE, 155MM, HE, RA, M549A1 AFT (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-63203-1983 PROJECTILE, 155MM, HE, RA, M549A1 AFT (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-70762 (2)-1996 PROPELLANT, COMPOSITE, CAST, FOR USE IN SIMULATOR, MISSILE: SAGGER XM27
• ARMY MIL-P-70762-1990 PROPELLANT, COMPOSITE, CAST, FOR USE IN SIMULATOR, MISSILE: SAGGER XM27
• ARMY MIL-T-63262 NOTICE 4-1997 TEST MODE ASSEMBLY, ROCKET: M180 CRATERING DEVICE PROPELLANT TESTING
• ARMY MIL-T-63262 REINST NOTICE 3-1996 TEST MODE ASSEMBLY, ROCKET: M180 CRATERING DEVICE PROPELLANT TESTING
• ARMY MIL-T-63262 VALID NOTICE 1-1991 TEST MODE ASSEMBLY, ROCKET: M180 CRATERING DEVICE PROPELLANT TESTING
• ARMY MIL-T-63262-1978 TEST MODE ASSEMBLY, ROCKET: M180 CRATERING DEVICE PROPELLANT TESTING
• ARMY MIL-P-50573 C (4)-1987 PROJECTILE, 155MM, HE, ROCKET ASSISTED M549& M549A1 FORWARD (AHH) PROPELLANT GRAIN FOR
• ARMY MIL-P-50573 C-1979 PROJECTILE, 155MM, HE, ROCKET ASSISTED M549& M549A1 FORWARD (AHH) PROPELLANT GRAIN FOR
• ARMY MIL-P-63202 NOTICE 1-1996 PROJECTILE, 155MM, HE, RA, M549A1 FORWARD (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-63202 (2)-1987 PROJECTILE, 155MM, HE, RA, M549A1 FORWARD (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-63202-1983 PROJECTILE, 155MM, HE, RA, M549A1 FORWARD (M37 EXTRUDED) PROPELLANT GRAIN FOR
• ARMY MIL-P-46252 C VALID NOTICE 1-1991 PROPELLANT, M1 FOR USE IN 105MM CARTRIDGE, HEP-T, M393A2, WP-T, M416 AND TP-T, M467

U.S. Air Force, propellant

• AIR FORCE MIL-P-87897 ADMIN. NOTICE 3-2005 PROPELLANT, DEUTERIUM
• AIR FORCE MIL-P-87897 VALID NOTICE 1-1988 PROPELLANT, DEUTERIUM
• AIR FORCE MIL-P-87897-1982 PROPELLANT, DEUTERIUM
• AIR FORCE MIL-PRF-27201 D-2007 PROPELLANT, HYDROGEN
• AIR FORCE MIL-PRF-27201 E-2013 PROPELLANT, HYDROGEN
• AIR FORCE MIL-PRF-7254 G-1997 PROPELLANT, NITRIC ACID
• AIR FORCE MIL-PRF-25508 G-2006 PROPELLANT, OXYGEN
• AIR FORCE MIL-PRF-26536 E (1)-2000 PROPELLANT, HYDRAZINE
• AIR FORCE MIL-PRF-26536 E-1997 PROPELLANT, HYDRAZINE
• AIR FORCE MIL-PRF-32207-2006 PROPELLANT, METHANE
• AIR FORCE MIL-P-87931 ADMIN NOTICE 2-2005 PROPELLANT, ISOPROPYL ALCOHOL
• AIR FORCE MIL-P-87931-1977 PROPELLANT, ISOPROPYL ALCOHOL
• AIR FORCE MIL-P-87931 VALID NOTICE 2-2010 Propellant, Isopropyl Alcohol
• AIR FORCE MIL-DTL-25576 E-2006 PROPELLANT, ROCKET GRADE KEROSENE
• AIR FORCE MIL-P-87896 ADMIN NOTICE 2-2005 PROPELLANT, NITROGEN TRIFLUORIDE
• AIR FORCE MIL-P-87896 (1)-1987 PROPELLANT, NITROGEN TRIFLUORIDE
• AIR FORCE MIL-P-87896-1982 PROPELLANT, NITROGEN TRIFLUORIDE
• AIR FORCE MIL-PRF-25604 E-1997 PROPELLANT, UNS-DIMETHYLHYDRAZINE
• AIR FORCE MIL-PRF-27404 C-1997 PROPELLANT, MONOMETHYLHYDRAZINE
• AIR FORCE MIL-PRF-87896 A-2011 PROPELLANT, NITROGEN TRIFLUORIDE
• AIR FORCE MIL-PRF-27404 D-2012 PROPELLANT, MONOMETHYLHYDRAZINE
• AIR FORCE MIL-PRF-27407 C-2006 PROPELLANT PRESSURIZING AGENT, HELIUM
• AIR FORCE MIL-PRF-27415 B-2007 PROPELLANT PRESSURIZING AGENT, ARGON
• AIR FORCE MIL-PRF-27401 G-2013 PROPELLANT PRESSURIZING AGENT, NITROGEN
• AIR FORCE MIL-PRF-27415 C-2013 PROPELLANT PRESSURIZING AGENT, ARGON
• AIR FORCE MIL-PRF-26539 F-2006 PROPELLANTS, DINITROGEN TETROXIDE
• AIR FORCE MIL-DTL-25576 E VALID NOTICE 1-2011 PROPELLANT, ROCKET GRADE KEROSENE
• AIR FORCE MIL-PRF-26539 F VALID NOTICE 1-2011 Propellants, Dinitrogen Tetroxide
• AIR FORCE MIL-PRF-87930 A-1997 PROPELLANT, HYDRAZINE-WATER (70% HYDRAZINE - 30% WATER)
• AIR FORCE MIL-PRF-87930 B-2013 PROPELLANT, HYDRAZINE ?WATER (70 % HYDRAZINE ?30 % WATER)
• AIR FORCE MIL-PRF-27402 C-1997 PROPELLANT, HYDRAZINE - UNS-DIMETHYLHYDRAZINE (50% N2H4 - 50% UDMH)
• AIR FORCE MIL-DTL-87107 E-2012 PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10
• AIR FORCE MIL-DTL-87107 D VALID NOTICE 1-2011 Propellant, High Density Synthetic Hydrocarbon Type, Grade JP-10
• AIR FORCE MIL-DTL-87173 B ADMIN NOTICE 2-2005 PROPELLANT, PRIMING FLUID, ALCM ENGINE, GRADE PF-1
• AIR FORCE MIL-DTL-87173 B-1998 PROPELLANT, PRIMING FLUID, ALCM ENGINE, GRADE PF-1
• AIR FORCE MIL-DTL-87107 D-2006 PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10

Danish Standards Foundation, propellant

• DS/EN 13938-1/AC:2006 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• DS/EN 13938-1:2004 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• DS/EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
• DS/EN 13938-2:2004 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy
• DS/EN 13938-5:2004 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• DS/EN 13938-7:2004 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder
• DS/EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration of detonation transition
• DS/EN 13938-4:2004 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions
• DS/EN 268:1991 Propellants for commercial ammunition. Requirements and test methods

Lithuanian Standards Office , propellant

• LST EN 13938-1-2005 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• LST EN 13938-1-2005/AC-2006 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• LST EN 13938-6-2004 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
• LST EN 13938-2-2005 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy
• LST EN 13938-7-2004 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder
• LST EN 13938-5-2005 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• LST EN 13938-3-2004 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition
• LST EN 13938-4-2004 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions

AT-ON, propellant

• OENORM EN 13938-1-2021 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• OENORM EN 13938-5-2021 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• OENORM EN 13938-2-2021 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic discharge
• OENORM EN 13938-7-2021 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of safe and reliable ignition and complete deflagration of black powder

European Committee for Standardization (CEN), propellant

• prEN 13938-1-2021 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants; Guide for the determination of integrity of inhibitor coatings
• EN 13938-7:2004 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder
• prEN 13938-2-2021 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic discharge
• prEN 13938-5-2021 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• EN 13938-5:2004 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• EN 13938-2:2004 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy
• prEN 13938-3-2021 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition
• prEN 13938-4-2021 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions
• EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration of detonation transition
• EN 13938-4:2003 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions
• EN 13938-1:2004 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• prEN 13938-7-2021 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of safe and reliable ignition and complete deflagration of black powder
• EN 268:1991 Propellants for commercial ammunition; requirements and test methods

AENOR, propellant

• UNE-EN 13938-1:2005 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements
• UNE-EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
• UNE-EN 13938-2:2005 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy
• UNE-EN 13938-7:2005 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder
• UNE-EN 13938-5:2005 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures
• UNE-EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition
• UNE-EN 13938-4:2004 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions

German Institute for Standardization, propellant

• DIN EN 13938-1:2005-01 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements; German version EN 13938-1:2004 / Note: To be replaced by DIN EN 13938-1 (2021-05).
• DIN EN 13938-1 Berichtigung 1:2006-08 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements; German version EN 13938-1:2004, Corrigenda to DIN EN 13938-1:2005-01; German version EN 13938-1:2004/AC:2006 / Note: To be replaced by DIN EN 13938-1 (2021-05).
• DIN EN 13938-1:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements; German and English version prEN 13938-1:2021 / Note: Date of issue 2021-04-16*Intended as replacement for DIN EN 13938-1 (2005-01), DIN EN 13938-1 Berichtigung 1 (20...
• DIN EN 13938-1:2005 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements; German version EN 13938-1:2004
• DIN EN 13938-6:2004-07 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings; German version EN 13938-6:2004
• DIN EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Part 6: Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings; German version EN 13938-6:2004
• DIN EN 13938-2:2005-01 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy; German version EN 13938-2:2004 / Note: To be replaced by DIN EN 13938-2 (2021-05).
• DIN EN 13938-7:2004 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder; German version EN 13938-7:2004
• DIN EN 13938-5:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures; German and English version prEN 13938-5:2021 / Note: Date of issue 2021-04-16*Intended as replacement for DIN EN 13938-5 (2004-11).
• DIN EN 13938-5:2004-11 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures; German version EN 13938-5:2004 / Note: To be replaced by DIN EN 13938-5 (2021-05).
• DIN EN 13938-7:2004-11 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of properties of black powder; German version EN 13938-7:2004 / Note: To be replaced by DIN EN 13938-7 (2021-05).
• DIN EN 13938-5:2004 Explosives for civil uses - Propellants and rocket propellants - Part 5: Determination of voids and fissures; German version EN 13938-5:2004
• DIN EN 13938-2:2005 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic energy; German version EN 13938-2:2004
• DIN EN 13938-3:2003-06 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition; German version EN 13938-3:2003 / Note: To be replaced by DIN EN 13938-3 (2021-05).
• DIN EN 13938-3:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition; German and English version prEN 13938-3:2021 / Note: Date of issue 2021-04-16*Intended as replacement for DIN EN 13938-3 (2...
• DIN EN 13938-2:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 2: Determination of resistance to electrostatic discharge; German and English version prEN 13938-2:2021 / Note: Date of issue 2021-04-16*Intended as replacement for DIN EN 13938-2 (2...
• DIN EN 13938-4:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions; German and English version prEN 13938-4:2021 / Note: Date of issue 2021-04-16*Intended as replacement for DIN EN 13938-4 (2...
• DIN EN 13938-4:2004-03 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions; German version EN 13938-4:2003 / Note: To be replaced by DIN EN 13938-4 (2021-05).
• DIN EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Part 3: Determination of deflagration to detonation transition; German version EN 13938-3:2003
• DIN EN 13938-4:2004 Explosives for civil uses - Propellants and rocket propellants - Part 4: Determination of burning rate under ambient conditions; German version EN 13938-4:2003
• DIN EN 13938-7:2021-05 Explosives for civil uses - Propellants and rocket propellants - Part 7: Determination of safe and reliable ignition and complete deflagration of black powder; German and English version prEN 13938-7:2021 / Note: Date of issue 2021-04-16*Intended as re...

ES-UNE, propellant

• UNE-EN 13938-1:2005/AC:2006 Explosives for civil uses - Propellants and rocket propellants - Part 1: Requirements

Association Francaise de Normalisation, propellant

• NF EN 13938-1:2005 Explosifs à usage civil - Poudres propulsives et propergols pour fusées - Partie 1 : exigences
• NF T70-938-1*NF EN 13938-1:2005 Explosives for civil uses - Propellants and rocket propellants - Part 1 : requirements.
• NF EN 13938-6:2004 Explosifs à usage civil - Poudres propulsives et propergols pour fusées - Partie 6 : propergols solides pour autopropulsion - Guide pour la détermination de l'intégrité des revêtements modérateurs
• NF T70-938-6*NF EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Part 6 : solid rocket propellants - Guide for the determination of integrity of inhibitor coatings.
• NF T70-938-7*NF EN 13938-7:2005 Explosives for civil uses - Propellants and rocket propellants - Part 7 : determination of properties of black powder.
• NF T70-938-5*NF EN 13938-5:2005 Explosives for civil uses - Propellants and rocket propellants - Part 5 : dermination of voids and fissures.
• NF T70-938-2*NF EN 13938-2:2005 Explosives for civil uses - Propellants and rocket propellants - Part 2 : determination of resistance to electrostatic energy.
• NF EN 13938-2:2005 Explosifs à usage civil - Poudres propulsives et progergols pour fusées - Partie 2 : détermination de la résistance à l'énergie électrostatique
• NF EN 13938-5:2005 Explosifs à usage civil - Poudres propulsives et propergols pour fusées - Partie 5 : détermination des creux et des crevasses
• NF T70-938-3*NF EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Part 3 : determination of deflagration to detonation transition.
• NF T70-938-4*NF EN 13938-4:2004 Explosives for civil uses - Propellants and rocket propellants - Part 4 : determination of burning rate under ambient conditions.
• NF EN 13938-4:2004 Explosifs à usage civil - Poudres propulsives et propergols pour fusées - Partie 4 : détermination de la vitesse de combustion dans les conditions ambiantes
• NF U66-051:1983 Appareils d'abattage à charge propulsive pyrotechnique - Règles générales
• NF EN 16264:2014 Articles pyrotechniques - Autres articles pyrotechniques - Cartouches pour outils à charge propulsive
• NF EN 15895/IN1:2018 Outils portatifs à charge propulsive - Exigences de sécurité - Outils de scellement et de marquage
• NF EN 15895+A1:2018 Outils portatifs à charge propulsive - Exigences de sécurité - Outils de scellement et de marquage
• NF U66-052:1990 Matériel des industries de la viande - Appareils d'abattage à charge propulsive pyrotechnique - Épreuves.

British Standards Institution (BSI), propellant

• BS EN 13938-6:2004 Explosives for civil uses - Propellants and rocket propellants - Solid rocket propellants - Guide for the determination of integrity of inhibitor coatings
• BS EN 13938-1:2004 Explosives for civil uses — Propellants and rocket propellants — Part 1: Requirements
• BS EN 13938-1:2004(2007) Explosives for civil uses — Propellants and rocket propellants — Part 1: Requirements
• BS EN 13938-2:2004 Explosives for civil uses - Propellants and rocket propellants - Determination of resistance to electrostatic energy
• BS EN 13938-7:2004 Explosives for civil uses - Propellants and rocket propellants - Determination of properties of black powder
• BS EN 13938-5:2004 Explosives for civil uses - Propellants and rocket propellants - Determination of voids and fissures
• 21/30423895 DC BS EN 13938-1. Explosives for civil uses. Propellants and rocket propellants - Part 1. Requirements
• BS EN 13938-4:2003 Explosives for civil uses - Propellants and rocket propellants - Determination of burning rate under ambient conditions
• BS EN 13938-3:2003 Explosives for civil uses - Propellants and rocket propellants - Determination of deflagration to detonation transition
• 21/30423901 DC BS EN 13938-5. Explosives for civil uses. Propellants and rocket propellants - Part 5. Determination of voids and fissures
• 21/30423898 DC BS EN 13938-3. Explosives for civil uses. Propellants and rocket propellants - Part 3. Determination of deflagration to detonation transition
• 21/30423883 DC BS EN 13938-2. Explosives for civil uses. Propellants and rocket propellants - Part 2. Determination of resistance to electrostatic discharge
• 21/30423937 DC BS EN 13938-4. Explosives for civil uses. Propellants and rocket propellants - Part 4. Determination of burning rate under ambient conditions
• 21/30423904 DC BS EN 13938-7. Explosives for civil uses. Propellants and rocket propellants - Part 7. Determination of safe and reliable ignition and complete deflagration of black powder
• BS ISO 23339:2011 Space systems. Unmanned spacecraft. Estimating the mass of remaining usable propellant

United States Navy, propellant

• NAVY MIL-P-81994 VALID NOTICE 1-1991 PROPELLANT FOR 20MM AMMUNITION
• NAVY MIL-P-81994-1975 PROPELLANT FOR 20MM AMMUNITION
• NAVY MIL-DTL-32298-2008 CASTING POWDER, PROPELLANT
• NAVY MIL-P-85364 A-1993 PROPELLANT, CTBN 23-17
• NAVY MIL-P-82691 A NOTICE 1-1992 PROPELLANT GRAIN, IGNITER
• NAVY MIL-P-82691 A-1989 PROPELLANT GRAIN, IGNITER
• NAVY MIL-P-82739 (1)-1988 PROPELLANT GRAINS, NOSOL-318
• NAVY MIL-P-82739-1985 PROPELLANT GRAINS, NOSOL-318
• NAVY MIL-G-82438 C NOTICE 1-1998 GRAIN, IGNITER, PROPELLANT
• NAVY MIL-G-82438 C-1984 GRAIN, IGNITER, PROPELLANT
• NAVY MIL-P-17449 NOTICE 1-1995 PROPELLANT, CORDITE-N
• NAVY MIL-P-17449 (2)-1972 PROPELLANT, CORDITE-N
• NAVY MIL-P-17449-1953 PROPELLANT, CORDITE-N
• NAVY MIL-P-19264 B-1993 PROPELLANT, BS-NACO, FOR THE 5"/54 CALIBER PROPELLING CHARGE
• NAVY MIL-DTL-82762 B-2004 CUTTER, DELAY, PROPELLANT ACTUATED, MLU-58/B
• NAVY MIL-DTL-82965 B-2001 PROPELLANT, GUN, HIGH ENERGY NITRAMINE
• NAVY MIL-DTL-32040-1999 PROPELLANT, GUN, HIGH ENERGY NITRAMINE
• NAVY MIL-P-82944 (1)-1997 PROPELLANT, SOLID COMPOSITE
• NAVY MIL-P-82944-1995 PROPELLANT, SOLID COMPOSITE
• NAVY MIL-I-81508 NOTICE 1-1996 INDICATOR PLUG, FOR MISSILE PROPELLANTS
• NAVY MIL-I-81508 (1)-1979 INDICATOR PLUG, FOR MISSILE PROPELLANTS
• NAVY MIL-I-81508-1966 INDICATOR PLUG, FOR MISSILE PROPELLANTS
• NAVY MIL-P-85759-1986 PROPELLANT GRAIN, MARK 93 MOD 0
• NAVY MIL-P-231 A NOTICE 1-1995 PROPELLANT, PYROCELLULOSE
• NAVY MIL-P-231 A (2)-1972 PROPELLANT, PYROCELLULOSE
• NAVY MIL-P-231 A-1955 PROPELLANT, PYROCELLULOSE
• NAVY MIL-P-18942 A NOTICE 2-1986 PROPELLANT FOR 20MM ANTI-AIRCRAFT GUN MARK 12
• NAVY MIL-P-18942 A (3)-1971 PROPELLANT FOR 20MM ANTI-AIRCRAFT GUN MARK 12
• NAVY MIL-P-18942 A NOTICE 1-1963 PROPELLANT FOR 20MM ANTI-AIRCRAFT GUN MARK 12
• NAVY MIL-P-18942 A-1956 PROPELLANT FOR 20MM ANTI-AIRCRAFT GUN MARK 12
• NAVY MIL-DTL-50374 B-2004 INITIATOR, PROPELLANT ACTUATED, M104 ASSEMBLY
• NAVY MIL-P-60852 A NOTICE 2-1999 PROPELLANT, GRAIN, INHIBITED
• NAVY MIL-P-60852 A VALID NOTICE 1-1991 PROPELLANT, GRAIN, INHIBITED
• NAVY MIL-P-60852 A-1970 PROPELLANT, GRAIN, INHIBITED
• NAVY MIL-P-17689 NOTICE 3-2003 PROPELLANT, DOUBLE-BASE SHEET, TYPE N-5
• NAVY MIL-P-17689 VALID NOTICE 1-1975 PROPELLANT, DOUBLE-BASE SHEET, TYPE N-5
• NAVY MIL-P-17689-1953 PROPELLANT, DOUBLE-BASE SHEET, TYPE N-5
• NAVY MIL-H-22251-1959 HYDRAZINE SOLUTION (22-PERCENT)
• NAVY MIL-DTL-50699 B-2005 INITIATOR, PROPELLANT ACTUATED, JAU-2/A25 ASSEMBLY
• NAVY MIL-DTL-50714 C-2004 INITIATOR, PROPELLANT ACTUATED, DELAY, M113 ASSEMBLY
• NAVY MIL-P-82887-1993 PROPELLANT, M6+2 FOR THE 76MM/62 CALIBER CARTRIDGE
• NAVY MIL-DTL-82960 A-2003 INITIATOR, PROPELLANT ACTUATED, JAU-27/A (MF72)
• NAVY MIL-DTL-85097 E (1)-2001 USN/USMC PROPELLANT ACTUATED DEVICES (PADS), GENERAL SPECIFICATION FOR
• NAVY MIL-DTL-85097 E SUPP 1-2000 USN/USMC PROPELLANT ACTUATED DEVICES (PADS), GENERAL SPECIFICATION FOR
• NAVY MIL-DTL-85097 E-2000 USN/USMC PROPELLANT ACTUATED DEVICES (PADS), GENERAL SPECIFICATION FOR
• NAVY MIL-P-22314 REINST NOTICE 2-1995 PROPELLANT, US NAVY GUNS, BALLISTIC APPENDIX
• NAVY MIL-P-22314 (3)-1971 PROPELLANT, US NAVY GUNS, BALLISTIC APPENDIX
• NAVY MIL-P-22314-1960 PROPELLANT, US NAVY GUNS, BALLISTIC APPENDIX
• NAVY MIL-G-85258-1981 GENERATOR, GAS PRESSURE, PROPELLANT ACTUATED BBU-18/B
• NAVY MIL-DTL-50375 B-2004 INITIATOR, PROPELLANT ACTUATED, M104 METAL PARTS ASSEMBLY
• NAVY MIL-P-85548 B-1990 PROPELLANT, COMPOSITE, CAST, N-60
• NAVY MIL-DTL-46992 E-2006 CUTTER, DELAY, PROPELLANT ACTUATED, M21 (2 SEC) AND M22 (10 SEC)
• NAVY MIL-E-19042-1955 ENGINE: ROCKET, SOLID PROPELLANT, 2.2 SECOND DURATION - 11,000 POUNDS THRUST
• NAVY MIL-E-19042 VALID NOTICE 1-1964 ENGINE: ROCKET, SOLID PROPELLANT, 2.2 SECOND DURATION - 11,000 POUNDS THRUST
• NAVY MIL-P-85661 VALID NOTICE 1-1991 PROPELLANT EXTRUDED, 25 MM, ARMOR PIERCING INCENDIARY (API), PGU-20/U
• NAVY MIL-P-85661-1985 PROPELLANT EXTRUDED, 25 MM, ARMOR PIERCING INCENDIARY (API), PGU-20/U
• NAVY MIL-P-85662 VALID NOTICE 1-1991 PROPELLANT, BALL, 25 MM, ARMOR PIERCING INCENDIARY (API), PGU-20/U
• NAVY MIL-P-85662-1985 PROPELLANT, BALL, 25 MM, ARMOR PIERCING INCENDIARY (API), PGU-20/U
• NAVY MIL-P-82522 C-1990 PROPELLANT, JET ENGINE, T-H DIMER, GRADE RJ-4
• NAVY MIL-DTL-50700 A-2005 INITIATOR, PROPELLANT ACTUATED, JAU-2/A25 METAL PARTS ASSEMBLY
• NAVY MIL-L-23822 C VALID NOTICE 1-1987 LIQUID PROPELLANT ROCKET ENGINE LR64 FOR AQM-37A MISSILE TARGET SYSTEM
• NAVY MIL-L-23822 C-1971 LIQUID PROPELLANT ROCKET ENGINE LR64 FOR AQM-37A MISSILE TARGET SYSTEM

Society of Automotive Engineers (SAE), propellant

• SAE AMS3015-1985 NITROGEN, LIQUID, PROPELLANT GRADE
• SAE AMS3012-1985 OXYGEN, LIQUID, PROPELLANT GRADE
• SAE AIR1343A-2007 Liquid Propellant Gas Generation Systems
• SAE AMS3010-1985 HYDROGEN, LIQUID, HIGH PURITY, PROPELLANT GRADE
• SAE AS8581-2000 Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust FSC 2845; Should Be Used Instead of MIL-E-8581A(AS), Which Was Cancelled on 26 May 2000
• SAE AIR839-1965 RECOMMENDED MATERIALS AND PRACTICES FOR USE WITH CRYOGENIC PROPELLANTS
• SAE AIR839B-1993 RECOMMENDED MATERIALS AND PRACTICES FOR USE WITH CRYOGENIC PROPELLANTS
• SAE AIR839C-2000 Recommended Materials and Practices for Use with Cryogenic Propellants
• SAE AIR1129-1999 Aerospace Ground Equipment Criteria for a Propellant Transfer Unit

SAE - SAE International, propellant

• SAE AMS3015-1965 Nitrogen@ Liquid Propellent Grade
• SAE AMS3012A-1990 OXYGEN@ LIQUID@ PROPELLANT GRADE
• SAE AMS3015A-1996 NITROGEN@ LIQUID@ PROPELLANT GRADE
• SAE AIR1343A-1992 Liquid Propellant Gas Generation Systems
• SAE AMS3010A-1990 HYDROGEN@ LIQUID@ HIGH PURITY@ PROPELLANT GRADE
• SAE AIR1343B-2013 Liquid Propellant Gas Generation Systems
• SAE AIR839C-1969 Recommended Materials and Practices for Use with Cryogenic Propellants
• SAE AIR839A-1967 RECOMMENDED MATERIALS AND PRACTICES FOR USE WITH CRYOGENIC PROPELLANTS
• SAE AIR839B-1969 Recommended Materials and Practices for Use with Cryogenic Propellants
• SAE AIR1129-1969 Aerospace Ground Equipment Criteria for a Propellant Transfer Unit
• SAE ARP1206A-2012 Aerospace Ground Equipment Criteria for Umbilical Systems Propellant Quick-Disconnects

Military Standard of the People's Republic of China-General Armament Department, propellant

• GJB 2257-1994 rocket propellant terminology
• GJB 682-1989 liquid propellant terminology
• GJB 9832-2020 Guidelines for safe use of xenon propellant for electric propulsion
• GJB 325-1987 Nomenclature rules for composite solid propellants
• GJB 325A-2021 Nomenclature rules for composite solid propellants
• GJB 9752-2020 Specification for ammonium dinitramide-based propellants
• GJB 9924-2021 Specifications for new mixed hydrazine (XT-1) propellant
• GJB 1501-1992 General analytical method for hydrazine propellants
• GJB 2301-1995 Liquid propellant container color markings
• GJB 9874-2020 Specification for gel propellant decomposition catalysts
• GJB 8985-2017 Spacecraft propellant tank series type spectrum
• GJB 171A-2021 Nomenclature rules for double-base solid propellants
• GJB 7335-2011 Bleed-off criterion for conventional propellants in spacecraft launching complex
• GJB 7911-2012 Rules for conventional propellants filling of spacecraft launch site
• GJB 7910-2012 Rules for cryogenic propellants filling of spacecraft launch site
• GJB 5845-2006 General specification for liquid propellant tank of titanic alloy
• GJB 5848-2006 Detection methods of propellant leak for satellite on launching site
• GJB 6762-2009 Bleed-off criterion for cryogenic propellants in spacecraft launching complex
• GJB/Z 84-1996 Thermodynamic calculation method of propellant energy characteristics
• GJB 4093-2000 Double-base propellant charge inspection and acceptance rules
• GJB 1474.3-1992 Propellant Usage Rules for Space Launch Site Liquid Hydrogen
• GJB 1474.4-1992 Propellant usage rules for space launch sites helium
• GJB 5218-2003 Changes in charging specifications for aluminum-lead high burning rate propellants
• GJB/J 5460-2005 Specification for burning rate reference materials for high burning rate propellants
• GJB 5287-2004 General Specification for Missile Propellant Sampling Transport Vehicles
• GJB 10022-2021 Constant strain test method for composite solid propellants
• GJB 10111-2021 Specification for spacecraft propellant replenishment gas compressors
• GJB/J 3346-1998 Calibration procedures for solid propellant specific impulse test systems
• GJB 1022-1990 General specifications for missile erection equipment (liquid propellant)
• GJB 1474.1-1992 Rules for the use of propellants at the space launch site anhydrous hydrazine
• GJB 10012-2021 Hazard classification method for composite solid propellants
• GJB 10021-2021 Composite solid propellant accelerated aging test method
• GJB 8734-2015 Specification for aniline cross-linking agents for hydroxyl butadiene propellant linings
• GJB 6763-2009 Safety criterion for cryogenic propellant system in space launching site
• GJB 2301-1995(XG1-2015) Liquid propellant container color marking revision sheet 1-2015
• GJB 1474.2-1992 Rules for the use of propellants at the space launch site: dimethylhydrazine
• GJB 7288-2011 General specification for filling flow monitoring equipmemt of missile propellant
• GJB/J 3348-1998 Calibration procedures for solid propellant smoke signal test systems
• GJB 1073A-2001 General specification for extrusion-formed double-base solid propellant charges
• GJB 1073-1991 General specification for extrusion-formed double-base solid propellant charges
• GJB 1073B-2019 General specification for extrusion-formed double-base solid propellant charges
• GJB 1073A-2000 General specification for extrusion-formed double-base solid propellant charges
• GJB 10-1984 Storing propellant liquid rocket engine test procedures
• GJB 10112-2021 Specifications for floating disconnectors of spacecraft propellant replenishment liquid (gas) circuits
• GJB 5219-2003 Specifications for diacetaldehyde and diacetaldehyde low burning rate propellant grains
• GJB 4699-1995*GJBz 20291.9-1995 Propellant filling equipment required for quality control of naval missile equipment
• GJB/Z 30-1992 Safety technical characteristics and management of composite solid propellant raw materials
• GJB 771.107-1993 Gunpowder performance test methods Solid propellant tensile strength test
• GJB/J 3346-1998(XG1-2015) Solid propellant specific impulse test system calibration regulations revision sheet 1-2015
• GJB 10018-2021 Composite solid propellant fixed load test and equilibrium modulus determination method
• GJB 9549-2018 Safety requirements for design of factories and warehouses for composite solid propellants and their products
• GJB 771.103-1989 Gunpowder performance test method Double base solid propellant powder shape and size measurement
• GJB 10032-2021 Safety technical characteristics and management requirements of composite solid propellant raw materials

North Atlantic Treaty Organization Standards Agency, propellant

• STANAG 6016-1996 SOLID PROPELLANT SMOKE CLASSIFICATION
• STANAG 4041-1960 SPECIFICATION FOR DNT (DINITROTOLUENE) FOR PROPELLANTS
• STANAG 4115-1997 DEFINITION AND DETERMINATION OF BALLISTIC PROPERTIES OF GUN PROPELLANTS
• STANAG 4581-2006 EXPLOSIVES; ASSESSMENT OF AGEING CHARACTERISTICS OF COMPOSITE PROPELLANTS CONTAINING AN INERT BINDER

Professional Standard - Aerospace, propellant

• QJ 1941-1990 Propellant Tank Design Guidelines
• QJ 2036-1991 Propellant combustion product temperature coefficient
• QJ 2215-1992 Composite solid propellant performance appraisal
• QJ 2482-1993 Nomenclature of composite solid propellant and charge
• QJ 1360-1988 Method for Determination of Hardness of Composite Solid Propellants
• QJ 2751-1995 Composite solid propellant non-destructive testing method
• QJ 3109-1999 Satellite liquid propellant safety testing regulations
• QJ 1360-1988修改单1-1996 Method for Determination of Hardness of Composite Solid Propellants
• QJ 3005-1998 Safety requirements for the use of storable liquid propellants
• QJ 2275-1992 Method for determination of specific heat capacity of composite solid propellant
• QJ 1113-1987 Composite solid propellant performance test sample
• QJ 3228-2005 Test method for Poisson's ratio of composite solid propellants
• QJ 20019-2011 Test method for safety performance of composite solid propellants
• QJ 924-1985 Composite solid propellant uniaxial tensile test method
• QJ 2328-1992 Composite solid propellant storage aging test method
• QJ 1616-1989 Method for Determination of Crosslinking Density of Composite Solid Propellant
• QJ 2913-1997 Method for Determination of Friction Sensitivity of Composite Solid Propellants
• QJ 1833-1990 General technical requirements for the manufacture and acceptance of propellant tanks
• QJ 925-1985 Test method for burning rate of composite solid propellant slurry
• QJ 3108-1999 Regulations on Safety Testing of Launch Vehicle Liquid Propellants
• QJ 3281-2006 Detection method of spacecraft propellant leakage at launch site
• QJ 20019.1-2011 Composite solid propellant safety performance test method
• QJ 20019.2-2011 Composite solid propellant safety performance test method
• QJ 20019.3-2011 Composite solid propellant safety performance test method
• QJ 20019.4-2011 Composite solid propellant safety performance test method
• QJ 1617-1989 Method for Determination of Glass Transition Temperature of Composite Solid Propellant
• QJ 1490-1988 Method for Determination of Linear Expansion Coefficient of Composite Solid Propellant
• QJ 1359-1988 Composite solid propellant detonation heat test method isothermal method
• QJ 2215A-2005 Composite solid propellant performance appraisal items and methods
• QJ 913A-1995 Analysis Method of Aluminum Powder Content in Composite Solid Propellant
• QJ 3214-2005 Safety evaluation for factory on research, development and production composite solid propellant
• QJ 20018-2011 Safety requirements for mechanical trimming of composite solid propellant grain
• QJ 3039-1998 Test method for drop weight impact sensitivity of composite solid propellants
• QJ 2216-1992 Composite solid propellant storage and transportation safety technical regulations
• QJ 2274-1992 Composite solid propellant development and production safety technical regulations
• QJ 1044A-2005 Test methods for storable propellant liquid rocket motors
• QJ 3234-2005 Management requirements for conventional liquid propellant safety protective equipment
• QJ 2328A-2005 High temperature accelerated aging test method for composite solid propellants
• QJ 2894-1997 Composite solid propellant development and production safety inspection rules
• QJ 913.5-1985 Composite solid propellant (polyether system) pH value determination method
• QJ 1627-1989 固体发动机
• QJ 1628-1989 固体发动机
• QJ 20049-2011 Anti-static safety rules for composite solid propellant development and production
• QJ 1814-1989 Standard Molar Enthalpy of Formation of Related Components of Composite Solid Propellants
• QJ 3256-2005 Process Safety Requirements for Development of High Burning Rate Hydroxybutylene Propellant
• QJ 1491.2-1988 固体发动机
• QJ 2117-1991 Specifications for liquid propellant slosh design of surface-to-surface missile launch vehicle
• QJ 1812-1989 Method for Determination of Initial Tensile Modulus of Composite Solid Propellants
• QJ 913.4-1985 Composite solid propellant (polyether system) - Method for determination of benzene extraction value
• QJ 1369-1988 General requirements for solid rocket motors for composite solid propellants
• QJ 1369A-2006 General requirements for solid rocket motors for composite solid propellants
• QJ 1591.1-1989 Composite solid propellant (butylated hydroxyl system) Iron oxide content analysis method
• QJ 914.4-1985 Composite solid propellant (butylene carboxyl system) - Analysis method for moisture content
• QJ 3144-2002 Determination for hazard classification and safe distance of composite solid propellant workshop building
• QJ 3208-2005 General specification for metal aneroid accummulator of rocket propellant transfer system
• QJ 912-1985 Underwater Acoustic Emission Determination Method of Burning Rate of Composite Solid Propellant Rod
• QJ 917-1985 固体发动机
• QJ 917A-1997 Method for determination of density of composite solid propellants and linings and insulation materials
• QJ 913.7-1985 Composite solid propellant (polyether system) Calcium carbonate content analysis method
• QJ 914.5-1985 Composite solid propellant (butylene carboxyl system) - Analytical method for residual styrene
• QJ 3188-2004 General specification for cryogenic propellant filling and venting and venting automatic disconnection connector
• QJ 809-1983 Method for determination of thermal conductivity of solid propellants and solid motor insulation
• QJ 809-1994 Quasi-steady-state method for the determination of thermal conductivity and specific heat capacity of composite solid propellants
• QJ 914.2-1985 Analytical method of ammonium perchlorate content in composite solid propellant (butylene carboxyl system)

US-MSFC, propellant

• MSFC NASA MPR 4500.1 REV C-2008 MANAGEMENT OF PROPELLANTS AND PRESSURANTS
• MSFC NASA MWI 8715.10 REV D-2008 EXPLOSIVES, PROPELLANT, AND PYROTECHNICS PROGRAM

GB-REG, propellant

• REG NASA-LLIS-0327-1993 Lessons Learned - Solid Propellant, Fire
• REG NASA-LLIS-0485-1996 Lessons Learned - Isolate the Propulsion Pressurization System from the Propellant Tanks (1993)
• REG NASA-LLIS-0328-1993 Lessons Learned - Solid Propellant, Electro-Static Discharge Ignition
• REG NASA-LLIS-0915-2000 Lessons Learned ?Propellant Management for Geosynchronous Satellite
• REG NASA-LLIS-0206-1992 Lessons Learned - Inertial Upper Stage (IUS) Propellant Tank Assemblies (PTA's)
• REG NASA-LLIS-1334-2003 Lessons Learned ?Cleanliness of Diaphragm Propellant Tanks (2000)
• REG NASA-LLIS-0168-1993 Lessons Learned - Hydrogen Detonation in Propellant Piping Systems
• REG NASA-LLIS-2196-2009 Lessons Learned - Hypergolic Propellant Related Spills and Fires
• REG NASA-LLIS-0344--1994 Lessons Learned - Solid Propellant in Contact with Porous Material, Fire
• REG NASA-STD 8719.12-2010 Safety Standard for Explosives, Propellants, and Pyrotechnics [Superseded: NASA NASA/NSS-1740.12]
• REG NASA-STD-8719.12 W/ CHG 2-2011 Safety Standard for Explosives, Propellants, and Pyrotechnics [Superseded: NASA NASA/NSS-1740.12]
• REG NASA-LLIS-1777-2007 Lessons Learned - COPV Propellant Tank Failure on the Dawn Spacecraft
• REG NASA-LLIS-0812-2000 Lessons Learned ?Leak Testing of Liquid Hydrogen and Liquid Oxygen Propellant Systems
• REG NASA-LLIS-0201-1992 Lessons Learned - Advanced Solid Rocket Motor (ASRM) Propellant Manufacturing Facility.
• REG NASA-LLIS-4058-2011 Lessons Learned - Use of Propellant Grade Commodities for Fuel Cell Powerplants

Aerospace Industries Association, propellant

• AIA NAS 3620-1983 Propellants, Nitrogen Tetroxide Rev. 1
• AIA NAS 1717-1967 Reliability Demonstration of Liquid Propellant Rocket Engines
• AIA NAS 1718-1967 Reliability Demonstration of Solid Propellant Rocket Motors

Aerospace Industries Association/ANSI Aerospace Standards, propellant

• AIA/NAS NAS3620-2013 PROPELLANTS, NITROGEN TETROXIDE Rev 2
• AIA/NAS NAS1718-2013 RELIABILITY DEMONSTRATION OF SOLID PROPELLANT ROCKET MOTORS Rev 1
• AIA/NAS NAS1717-2013 RELIABILITY DEMONSTRATION OF LIQUID PROPELLANT ROCKET ENGINES Rev 1

BE-NBN, propellant

• NBN-EN 268-1992

AIA/NAS - Aerospace Industries Association of America Inc., propellant

• NAS3620-2013 PROPELLANTS@ NITROGEN TETROXIDE (Rev 2)
• NAS1717-1967 Reliability Demonstration of Liquid Propellant Rocket Engines
• NAS1718-1967 Reliability Demonstration of Solid Propellant Rocket Motors
• NAS1717-2013 Reliability Demonstration of Liquid Propellant Rocket Engines (Rev 1)
• NAS1718-2013 RELIABILITY DEMONSTRATION OF SOLID PROPELLANT ROCKET MOTORS (Rev 1)

General Administration of Quality Supervision, Inspection and Quarantine of the People‘s Republic of China, propellant

• GB 14374-1993 Discharge standard of water pollutant and standard of analytical methed for space propellant
• GB/T 34523-2017(英文版) Estimating methods for the mass of remaining propellant of spacecraft
• GB/T 32295-2015 Design requirements for residual propellant venting of launch vehicle
• GB/T 32295-2015(英文版) Design requirements for residual propellant venting of launch vehicle

国家市场监督管理总局、中国国家标准化管理委员会, propellant

• GB/T 40536-2021 Design requirements for residual propellant venting of Spacecraft

Professional Standard - Military and Civilian Products, propellant

• WJ 2383-1997 General specification for wooden boxes for solid propellant packaging
• WJ 2640-2004 Specifications for reference materials of energetic materials for NEPE propellants

未注明发布机构, propellant

• GJB 2373-1995 Monitoring method for hydrazine propellant content in air
• BS EN 268:1991(1999) Specification for Propellants for commercial ammunition — Requirements and test methods
• GJB 10015.1-2021 Methods for assessing low vulnerability of solid propellants Part 1: General principles
• GJB 10A-2004 Storing propellant liquid rocket engine test projects and requirements
• BS ISO 23339:2010 Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
• GJB 10015.6-2021 Low vulnerability assessment method for solid propellants Part 6: Explosion test

Military Standard of the People's Republic of China-Commission of Science,Technology and Industry for National Defence, propellant

• GJB 6195-2008 Classification method for hazard grade of composite solid propellants
• GJB/J 5458-2005 Verificationg regulation for burning instrument of target line method of solid propellants
• GJB 6257-2008 Specification for aniline linking-agent of HTPB propellant liner

中华人民共和国国家质量监督检验检疫总局、中国国家标准化管理委员会, propellant

• GB/T 34523-2017 Estimating methods for the mass of remaining propellant of spacecraft

IN-BIS, propellant

• IS 10994 Pt.6-1985

American Society for Testing and Materials (ASTM), propellant

• ASTM F1750-16(2020) Standard Specification for Paintball Marker Threaded-Propellant Source Interface
• ASTM D2507-93 Standard Terminology of Rheological Properties of Gelled Rocket Propellants
• ASTM F309-04(2018) Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants
• ASTM F309-70(1996) Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants
• ASTM F309-18 Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants
• ASTM D2884-93(1998) Standard Test Method for Yield Stress of Heterogeneous Propellants by Cone Penetration Method
• ASTM D2508-93 Standard Test Method for Solid Rocket Propellant Specific Impulse Measurements
• ASTM F590-05 Consumer Safety Specification for Non-Powder Gun Projectiles and Propellants
• ASTM F590-12 Standard Consumer Safety Specification for Non-Powder Gun Projectiles and Propellants
• ASTM F590-92(2000) Consumer Safety Specification for Non-Powder Gun Projectiles and Propellants
• ASTM F590-12(2018) Standard Consumer Safety Specification for Non-Powder Gun Projectiles and Propellants
• ASTM D2540-93 Standard Test Method for Drop-Weight Sensitivity of Liquid Monopropellants
• ASTM F3344-19 Standard Guide for Storage, Use, and Handling of Liquid Rocket Propellants
• ASTM F590-22 Standard Consumer Safety Specification for Non-Powder Gun Projectiles and Propellants
• ASTM D2540-93(2001) Standard test method for drop weight sensitivity of liquid monocomponent propellants
• ASTM F309-04 Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants
• ASTM F309-04(2010) Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants
• ASTM D2884-93(2007) Standard Test Method for Yield Stress of Heterogeneous Propellants by Cone Penetration Method
• ASTM D2884-93(2012) Standard Test Method for Yield Stress of Heterogeneous Propellants by Cone Penetration Method

International Organization for Standardization (ISO), propellant

• ISO 14951-7:1999 Space systems - Fluid characteristics - Part 7: Hydrazine propellant
• ISO 14951-2:1999 Space systems - Fluid characteristics - Part 2: Hydrogen propellant
• ISO 14951-8:1999 Space systems - Fluid characteristics - Part 8: Kerosene propellant
• ISO 14951-6:1999 Space systems - Fluid characteristics - Part 6: Monomethylhydrazine propellant
• ISO 14951-5:1999 Space systems - Fluid characteristics - Part 5: Nitrogen tetroxide propellant
• ISO 14951-7:1999/Cor 1:2004 Space systems - Fluid characteristics - Part 7: Hydrazine propellant; Technical Corrigendum 1
• ISO 23339:2010 Space systems - Unmanned spacecraft - Estimating the mass of remaining usable propellant

Professional Standard - Navy, propellant

• HJB 384.6-2007 Liquid Propellant Analysis Procedures Part 6: Yutui-3
• HJB 384.4-2007 Liquid Propellant Assay Analysis Protocol Part 4: Nitric Acid-20S
• HJB 384.5-2007 Liquid propellants analytical procedures part 5: Mixed amine-50
• HJB 384.1-2007 Liquid propellant analytical procedures part 1: general requirements
• HJB 384.3-2007 Liquid Propellant Analysis Protocol Part 3: T-10 Fuel Oil
• HJB 384.2-2007 Liquid Propellant Assay Analysis Protocol Part 2: Jet Fuel No. 3

Professional Standard - Light Industry, propellant

• QB/T 4955-2016 Domestic sanitary insecticide-Insecticide aerosol propellant-Propane and butane

NATO - North Atlantic Treaty Organization, propellant

• STANAG 4098-1984 Procedures for the Determination of Propellant Charge Temperature Corrections (ED 3 AMD 0)
• STANAG 4115-1970 Definition and Determination of Ballistic Properties of Gun Propellants (ED 1 AMD 0; To obtain please contact your national Defense Standardization Office or the NATO Standardization Office website: http:/ so.nato.int so@ Phone: +32 (0)2 – 707 5556@ email

GOSTR, propellant

• GOST R 58655-2019 Agricultural mobile machinery. Rates for force produced by propelling agents on soil
• GOST R 58656-2019 Agricultural mobile machinery. Methods for determining force produced by propelling agents on soil

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