QJ 1392A-2005 in English
VALIDInternal-pressure test method for the chamber case of solid rocket motor
- Issued on:2005-12-12
- Implemented on:2006-05-01
- File Format:PDF
- Delivery:Via email within 1~3 business days
$243.00
1 Scope
This standard specifies the site requirements, equipment requirements, preparation before test, specimen assembly, procedures and data processing methods in the internal-pressure test for the chamber case of solid rocket motor.
This standard is applicable to hydraulic test, hydraulic burst test and positive pressure airtightness test of chamber case ("case" for short) of solid rocket motor ("motor" for short).
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), 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 of the normative document referred to applies.
GB/T 254 Semi-refined paraffin wax
GB 446 Fully refined paraffin wax
GB/T 678 Chemical reagent - Ethanol
GB/T 1227 Accurate pressure gauge
GB 1790 Medicinal vaseline
GB/T 6026 Acetone for industrial use
QJ 1275 Evaluation of uncertainty in measurement of solid rocket motor
QJ 2472.2 General technical specifications for lifting device—Cord lifting device
HG/T 2492 Ethyl-ɑ-cyanoacrylate instantaneous adhesives
3 Test site requirements
3.1 Test site requirements for hydrostatic test and hydraulic burst test
3.1.1 General
Generally, the test site shall have independent test bay, isolating operation room and test operation room.
3.1.2 Test bay
The test bay shall meet the following requirements:
a) It shall have observation, ventilation, lighting, power supply and other facilities;
b) It shall have enough area and space for assembly, disassembly, turnover and testing;
c) It shall have lifting and turning facilities;
d) The test bay shall be equipped with explosion-proof measures or load-bearing test pits with explosion-proof capability;
e) It shall have a good drainage system and a sewage treatment device according to the actual situation.
3.1.3 Isolating operation room
The isolating operation room shall meet the following requirements:
a) It shall have power supply;
b) It shall have lighting and observation facilities.
3.1.4 Test operation room
The test operation room shall meet the following requirements:
a) Temperature: 10°C to 30°C; relative humidity: ≤80%;
b) There shall be no strong vibration, electromagnetic or other interference;
c) The power supply shall be separated from the power supply of the test bay, with lighting equipment and grounding facilities.
3.2 Test site requirements for positive pressure airtightness test
Test sites shall generally meet the requirements of a), b) and c) in 3.1.2.
Foreword i
1 Scope
2 Normative references
3 Test site requirements
4 Test system composition
5 Test equipment
6 Preparation before test
7 Specimen assembly
8 Test procedures
9 Processing of test data
10 Test report
Annex A (Informative) Formula of wax sealing ingredients
Annex B (Informative) Record tables formats

Loading PDF document...
Error loading PDF. Please make sure the file is valid and try again.
We also recommend
-

QJ 924-1985 in English
Uniaxial Tensile Test Methods for Composite Solid Propellant
1985-12-01 -

QJ 2893-1997 in English
Safety Requirements of Engine Test of Liquid Rocket
1997-03-19 -

QJ 1275-1994 in English
Evaluation of measurement uncertainty of solid rocket motor
1994-03-26 -

QJ 1617-1989 in English
Determination of glass transition temperature of composite solid propellant
1989-01-09 -

QJ 2609-1994 in English
High-energy X-ray Flaw Detection Method for Combustion Chamber in Solid Rocket Motor
1994-03-26 -

QJ 3083-1999 in English
Design Code for Gas Generator of Liquid Rocket Engine
1999-02-18 -

QJ 914.2-1985 in English
Analysis Method for Ammonium Perchlorate Content in Composite Solid Propellant (Carboxyl System)
1985-07-01 -

QJ 3005-1998 in English
Safety Requirements for Using of Storable Liquid Propellant
1998-02-06 -

QJ 1783A-1996 in English
General Specifications for Cavitation Venturi of Liquid Rocket Engine
1996-03-21 -

QJ 2338A-2002 in English
Storage test method for solid rocket motor
2002-11-20