This standard specifies terms and definitions of launch vehicle (LV) in aspects of universal purpose, systems, trajectory, loads and dynamic characteristics, aerodynamics, aerodynamic heating, mechanical environment, thermal environment, electromagnetic environment, natural environment, structure system, separation system, engine, pressurization and feeding system, control system, measurement system, propellant utilization system, failure detection and processing system, escape system, power supply and distribution system, ground test-launch-control system, launch site and integration assembly, and test and launch process flow.
This standard is applicable to LV development, including design, manufacture, test and launch, etc.
定价: 1116元 / 折扣价: 949 元 加购物车
This part of GB/T 34509 specifies the general requirements,data acquisition,technical process,calculation method,uncertainty analysis and other contents of in-orbit field radiometric calibration for visible-near infrared remote sensor of land observation satellite.
This part is applicable to in-orbit field radiometric calibration for visible-near infrared remote sensor of land observation satellite (hereinafter referred to as in-orbit field radiometric calibration)and can serve as a reference for similar remote sensors of other types of satellites.
定价: 252元 / 折扣价: 215 元 加购物车
This standard specifies the test requirements,test system,test procedures,test interruption and treatment as well as test result evaluation of the vibration test for spacecraft.
This standard is applicable to the system-level spacecraft vibration test,and can also serve as a reference for the vibration test of spacecraft at subsystems level and components level.
定价: 288元 / 折扣价: 245 元 加购物车