Efficiency of using low thrust throttleable rocket engines for carrying out near-earth orbit transfers
Saved in:
| Date: | 2018 |
|---|---|
| Main Authors: | B. N. Kiforenko, Ju. Vasilev, Ja. V. Tkachenko |
| Format: | Article |
| Language: | English |
| Published: |
2018
|
| Series: | International Scientific Technical Journal «Problems of Control and Informatics» |
| Online Access: | http://jnas.nbuv.gov.ua/article/UJRN-0001243719 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Journal Title: | Library portal of National Academy of Sciences of Ukraine | LibNAS |
Institution
Library portal of National Academy of Sciences of Ukraine | LibNASSimilar Items
-
Increasing the efficiency of combined control of the rocket engine thrust vector
by: Pryadko, N.S., et al.
Published: (2019) -
Using the Modified Method of Carrying Trajectory in Optimization of Interplanetary Transfers with Combination of High- and Low-Thrust
by: A. M. Kharitonov
Published: (2013) -
Comparative analysis of the efficiency of constant power throttled rocket engines for interorbital flights to geostationar
by: Ju. Vasilev, et al.
Published: (2021) -
Optimization of flights of the spacecrafts with electro-rocket engines
by: Ja. V. Tkachenko
Published: (2014) -
The place of an agreement on carrying out exploration works in the system of the agreements on carrying out work
by: V. K. Hutsuliak
Published: (2016)