Functions & application requirements for test launch and control system of ground to ground missile
1 Scope
This standard specifies the functions & application requirements such as basic composition, basic functions, design requirements, working modes, test items and methods and system-level tests of test launch and control system of ground to ground missile.
This standard is applicable to the design and application of the test launch and control system of ground-to-ground missile, and serves as a reference for the test launch and control system of launch vehicle.
2 Normative references
The following normative documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated reference, subsequent amendments to (excluding any corrigendum), or revisions of, any of these publications do not apply. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the latest editions of the standards indicated below. For undated references, the latest edition of the document referred to applies.
GJB 3470 Terms for missile ground equipments
GJB 3588 Terms for missile control system
3 Terms and definitions
For the purposes of this standard, the terms and definitions given in GJB 3470 and GJB 3588, as well as the following apply.
3.1
low voltage state
state when power safety test current is applied to test the time sequence of initiating explosive device bus on the missile without power conversion
3.2
high voltage state
state when rated working voltage (including deviation) is applied to test the time sequence of initiating explosive device bus on the missile after power conversion
4 Design basis
4.1 Comprehensive design assignment of control system.
4.2 Comprehensive design assignment of test launch and control system.
4.3 Environmental conditions for application of ground equipment.
4.4 Control system reliability outline, safety outline, maintainability outline, electromagnetic compatibility outline and integrated standardization requirements, etc.
5 Composition, function and design requirements for test launch and control system
Foreword i 1 Scope 2 Normative references 3 Terms and definitions 4 Design basis 5 Composition, function and design requirements for test launch and control system 6 Working mode and basic operation 7 Test item and state 8 System test
Functions & application requirements for test launch and control system of ground to ground missile
1 Scope
This standard specifies the functions & application requirements such as basic composition, basic functions, design requirements, working modes, test items and methods and system-level tests of test launch and control system of ground to ground missile.
This standard is applicable to the design and application of the test launch and control system of ground-to-ground missile, and serves as a reference for the test launch and control system of launch vehicle.
2 Normative references
The following normative documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated reference, subsequent amendments to (excluding any corrigendum), or revisions of, any of these publications do not apply. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the latest editions of the standards indicated below. For undated references, the latest edition of the document referred to applies.
GJB 3470 Terms for missile ground equipments
GJB 3588 Terms for missile control system
3 Terms and definitions
For the purposes of this standard, the terms and definitions given in GJB 3470 and GJB 3588, as well as the following apply.
3.1
low voltage state
state when power safety test current is applied to test the time sequence of initiating explosive device bus on the missile without power conversion
3.2
high voltage state
state when rated working voltage (including deviation) is applied to test the time sequence of initiating explosive device bus on the missile after power conversion
4 Design basis
4.1 Comprehensive design assignment of control system.
4.2 Comprehensive design assignment of test launch and control system.
4.3 Environmental conditions for application of ground equipment.
4.4 Control system reliability outline, safety outline, maintainability outline, electromagnetic compatibility outline and integrated standardization requirements, etc.
5 Composition, function and design requirements for test launch and control system
Contents of QJ 2149A-2008
Foreword i
1 Scope
2 Normative references
3 Terms and definitions
4 Design basis
5 Composition, function and design requirements for test launch and control system
6 Working mode and basic operation
7 Test item and state
8 System test
