Comparative analysis of the efficiency of constant power throttled rocket engines for interorbital flights to geostationar
Saved in:
| Date: | 2021 |
|---|---|
| Main Authors: | Ju. Vasilev, B. N. Kiforenko, Ja. V. Tkachenko |
| Format: | Article |
| Language: | English |
| Published: |
2021
|
| Series: | International Scientific Technical Journal «Problems of Control and Informatics» |
| Online Access: | http://jnas.nbuv.gov.ua/article/UJRN-0001298729 |
| 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
Dynamic instability of rockets deflectors in flight
by: Чернобрывко, М. В., et al.
Published: (2014)
by: Чернобрывко, М. В., et al.
Published: (2014)
Similar Items
-
Optimization of flights of the spacecrafts with electro-rocket engines
by: Ja. V. Tkachenko
Published: (2014) -
Efficiency of using low thrust throttleable rocket engines for carrying out near-earth orbit transfers
by: B. N. Kiforenko, et al.
Published: (2018) -
Dynamic instability of rockets deflectors in flight
by: M. V. Chernobryvko, et al.
Published: (2014) -
Optimization of a maneuver of a small change of an orbit inclination angle of the interorbital transport vehicle with a propulsion system of limited power and energy accumulator
by: Ja. V. Tkachenko, et al.
Published: (2020) -
Dynamic instability of rockets deflectors in flight
by: Чернобрывко, М. В., et al.
Published: (2014)