1 Scope
This standard specifies the general requirements, characterization items and methods for chemical, physical and interfacial bonding performance characterization of composite solid propellant.
This standard is applicable to the characterization for different performances of composite solid propellant.
2 Normative references
The following normative documents contain provisions which, through reference in this standard, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply to this standard. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition applies.
GJB/Z 84-1996 Thermodynamics calculate method of propellant performance capability
GJB 97 Technical requirements and data processing of standard testing motor
GJB 770A-1997 Propellant test method
GJB 772A-1997 Explosive test method
GJB 2365-1995 Solid rocket motor—measuring method for static firing test
QJ 1360 Determination of hardness of composite solid propellant
QJ 1393 Thermodynamic calculation method and computer program of solid rocket motor
QJ 1468 Test method for initial thermal decomposition temperature and deflagration temperature of composite solid propellant
QJ 1469 Test method for electrostatic spark sensitivity of composite solid propellant and other explosives
QJ 1490 Determination of linear expansion factor of composite solid propellant
QJ 1813
(all parts) Determination methods for viscosity and pot life of composite solid propellant slurry
QJ 2275 Determination of specific heat capacity of composite solid propellant
QJ 2328 Test method for temperature accelerated aging of
composite solid propellant
QJ 3228 Test method for Poisson’s ratio of composite solid propellant
3 General requirements
3.1 The raw materials for performance characterization of composite solid propellant shall comply with relevant standards and relevant technical documents. The performance characterization of propellant shall be carried out in the finalization stage.
3.2 The formula and manufacturing process of composite solid propellant samples for performance characterization shall be consistent with those of finalized propellant.
3.3 The characterization organization shall prepare the performance characterization report of composite solid propellant.
3.4 The performance characterization of composite solid propellant shall be conducted in accordance with the characterization items and methods specified in Clause 4. Other special items shall be carried out in accordance with the task book.
3.5 The characterization items of composite solid propellant are classified into mandatory items and optional items. The mandatory items are applicable to the performance characterization of all kinds of composite solid propellant. The optional items may be chosen by the supplier and the purchaser through negotiation in accordance with the characteristics and uses of specific propellants.
Foreword i
1 Scope
2 Normative references
3 General requirements
4 Characterization items and methods
