FIELD: aircraft engineering.
SUBSTANCE: invention can be used in contact less transportation of space objects in orbit. Spacecraft is placed in initial design orbit with ionic gun provided with gas discharge chamber with flat inductor to excite induction HF electric discharge, engine composed of electrical rocker engine (ERE), articulation with bars and hinges, a gimbal joint for displacement of ERE in the plane perpendicular to axis extending through spacecraft gravity centre in direction of ionic gun thrust vector. Spacecraft is brought closer and oriented relative to trailed spacecraft with the help of changing the thrust vector and trailed ERE thrust vector application point. Trailed spacecraft coordinates are measured as well as spacing between both craft. Trailed craft surface is subjected to effects of quasineutral ion beam by ion gun. Disturbing forces and moments acting on spacecraft are dynamically compensated. Spacecraft dynamic orientation is changed relative to trailed craft. Trained spacecraft is displace to disposal orbit Spacecraft is displaced in helical orbit in orbit the next trailed spacecraft.
EFFECT: higher efficiency of contactless transportation of spacecraft.
14 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF CONTROLLING SERVICE SPACECRAFT IN CONTACTLESS REMOVAL OF FRAGMENTS OF SPACE DEBRIS | 2019 |
|
RU2720606C1 |
METHOD OF STABILIZATION OF ANGULAR MOTION OF AN UNCOOPERATIVE OBJECT DURING CONTACTLESS TRANSPORTATION | 2018 |
|
RU2684022C1 |
SPACECRAFT FOR CLEANING NEAR-EARTH SPACE FROM SPACE DEBRIS | 2022 |
|
RU2784740C1 |
MODULE OF SPACECRAFT ENGINE PLANT (VERSIONS) | 2004 |
|
RU2271966C2 |
DEVICE FOR PROTECTION OF SPACECRAFT FROM SCATTERED PARTICLES FROM SURFACE OF IRRADIATED OBJECT | 2018 |
|
RU2688561C1 |
PULSED PLASMA ELECTRIC JET ENGINE | 2017 |
|
RU2720602C2 |
BIDIRECTIONAL WAVE PLASMA ENGINE FOR A SPACE VEHICLE | 2020 |
|
RU2764823C1 |
METHOD AND DEVICE FOR REGULATING THRUST VECTOR OF ELECTRIC ROCKET ENGINE | 2000 |
|
RU2196396C2 |
METHOD TO CONTROL MOVEMENT OF SERVICE SPACECRAFT | 2019 |
|
RU2714475C1 |
CONTROL SYSTEM OF ELECTRICAL ROCKET ENGINE | 2014 |
|
RU2564154C1 |
Authors
Dates
2015-11-20—Published
2014-08-25—Filed