FIELD: engines and pumps.
SUBSTANCE: proposed method consists in checking combined operation of CCS and RTES arranged in vacuum chamber by checking generated telemetry parametres and actual measured parametres of RTES actuators for compliance with generated control signals. Note here that RTES actuator parametre metres are arranged in vacuum chamber, while data generated by said metres is sent via uptight connector assembly to control computer.
EFFECT: maximum compliance of impedance characteristics of power lines from CCS to RTES, higher reliability of tests.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF TESTING ELECTROMAGNETIC COMPATIBILITY OF ELECTRIC PROPULSION SYSTEM WITH INFORMATION ONBOARD SYSTEMS OF SPACE OBJECT, SYSTEM OF RECORDING AND PLAYBACK OF CHARACTERISTICS OF DISCHARGE CURRENT OF ELECTRIC PROPULSION ENGINES OF ELECTRIC PROPULSION SYSTEM FOR IMPLEMENTING SAID METHOD | 2015 |
|
RU2605277C2 |
METHOD OF HEAT AND VACUUM TESTS OF THERMOCATALYTIC ENGINES WITHIN SPACECRAFT | 2012 |
|
RU2553587C2 |
METHOD AND DEVICE FOR MEASURING THRUST OF ELECTRIC JET ENGINES | 2006 |
|
RU2312316C1 |
METHOD FOR REDUCTION OF INTENSITY OF EFFECT OF SPREADING OF MATERIAL IN VACUUM CHAMBER IN TESTS OF ELECTRIC JET ENGINES AND SYSTEM FOR ITS IMPLEMENTATION | 2018 |
|
RU2688870C1 |
ELECTROJET PROPULSION DEVICE AND METHOD FOR MONITORING AND CONTROL OF TEMPERATURE IN ELECTROJET ENGINE WITH MAGNETISATION COILS | 2007 |
|
RU2370668C2 |
DEVICE FOR GROUND TESTING OF PNEUMATIC SYSTEM OF ELECTRIC ROCKET ENGINE INSTALLATION | 1994 |
|
RU2097601C1 |
ELECTRIC PROPULSION PLANT AND METHOD FOR ITS OPERATION | 2023 |
|
RU2805646C1 |
CONTROL SYSTEM OF ELECTRICAL ROCKET ENGINE | 2014 |
|
RU2564154C1 |
METHOD OF ORBITING SPACECRAFT FROM TRANSFER ORBIT TO GEOSTATIONARY ORBIT | 2009 |
|
RU2408506C1 |
UNIFIED SPACE PLATFORM MODULAR PRINCIPLE OF BUILDING | 2018 |
|
RU2684877C1 |
Authors
Dates
2011-03-10—Published
2009-12-16—Filed