GJB 4013A-2005
Testing and launching rules for three-stage rocket of LOX/LH engine (English Version)

Standard No.

GJB 4013A-2005

Language

Chinese, Available in English version

Release Date

2005

Published By

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

Status

Be replaced 2017-12

Replace By

GJB 4013B-2017

Latest

GJB 4013B-2017

Replace

GJB 4013-2000

Scope

This standard specifies the testing, transportation, hoisting, filling, launching and other working procedures and related procedures of three-stage carrier rockets with hydrogen and oxygen stages (CZ-3A, CZ-3B, CZ-3C, etc., hereinafter referred to as rockets) at the launch center. skills requirement. This standard applies to the test launch of rockets at the launch center, and the joint training of rockets at the launch center can also be implemented as a reference.

GJB 4013A-2005 Referenced Document

• GJB 2252-1994 Guidelines for safe application of dinitrogen tetroxide
• GJB 2253-1994 Guidelines for safe use of nitrogen and liquid nitrogen
• GJB 2990-1997 Guidelines for safe application of liquid oxygen
• GJB 4014-2000 Guidelines for safe use of helium
• GJB 5404-2005 Unsymmetrical dimethylhydrazine safe application rules
• GJB 5405-2005 Glossary of term:space nuclear power system with thermionic reactor*， 2005-12-12 Update

GJB 4013A-2005 history

• 2017 GJB 4013B-2017 Test and launch procedures for hydrogen and oxygen three-stage carrier rockets
• 2005 GJB 4013A-2005 Testing and launching rules for three-stage rocket of LOX/LH engine
• 2000 GJB 4013-2000 Test and launch procedures for hydrogen and oxygen three-stage carrier rockets

GJB 4013A-2005 Testing and launching rules for three-stage rocket of LOX/LH engine has been changed from GJB 4013-2000 Test and launch procedures for hydrogen and oxygen three-stage carrier rockets.