2017
DOI: 10.1016/j.actaastro.2017.05.018
|View full text |Cite
|
Sign up to set email alerts
|

Improving of technical characteristics of launch vehicles with liquid rocket engines using active onboard de-orbiting systems

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
7
0

Year Published

2018
2018
2023
2023

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 11 publications
(7 citation statements)
references
References 1 publication
0
7
0
Order By: Relevance
“…This analysis includes a description of all hazards associated with the operation in normal and accidental situations. For example, since 2010, each new design of a European launch vehicle has required a hazard analysis (Delorme and Biard, 2016;Pelton, 2016;Trushlyakov and Shatrov, 2017).…”
Section: Resultsmentioning
confidence: 99%
“…This analysis includes a description of all hazards associated with the operation in normal and accidental situations. For example, since 2010, each new design of a European launch vehicle has required a hazard analysis (Delorme and Biard, 2016;Pelton, 2016;Trushlyakov and Shatrov, 2017).…”
Section: Resultsmentioning
confidence: 99%
“…In accordance with the formulated concept of improving the ecological safety of LV with the main LPE [10,11,20,22], it is proposed to develop an additional ABDS, which is assigned the main part to ensure the specified indicators for the ecological safety of LV in the WS impact area:…”
Section: Development Of Ias Iamentioning
confidence: 99%
“…One of the important classes of such problems are the initial-boundary value problems for fourth order partial differential equations. To date, various methods for researching and solving the initial-boundary value problems for fourth order partial differential equations of hyperbolic and composite types are developed in [1][2][3][4][5][6][7][8][9][10][11][12]. In order to investigate various boundary value problems for fourth order partial differential equations along with the classical methods of mathematical physics (the Fourier method, the method of Green's functions, Poincare's metric concept) we apply the method of differential inequalities and other methods of qualitative theory of ordinary differential equations.…”
Section: Interaction Of Ias CD and Ias Lvmentioning
confidence: 99%
See 1 more Smart Citation
“…Space shuttle launches still largely involve carbon-based propellants. Greener launching methods are expected in the near future; liquid hydrogen may create new prospects [7].…”
mentioning
confidence: 99%