Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5145232 | International Journal of Hydrogen Energy | 2017 | 10 Pages |
Abstract
Findings on chilldown and fueling of the 12KRB upper stage may be used to verify calculation models while designing and developing the KVTK advanced upper stage with the lox/liquid hydrogen engine RD0146 of the Angara-A5V heavy class launch vehicle.
Related Topics
Physical Sciences and Engineering
Chemistry
Electrochemistry
Authors
A.G. Galeev, V.P. Firsov, I.V. Antyukhov, A.V. Galeev,