9. On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain
|
9. On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain |
| Pozdeyev G. L., Gamaza А. Е.
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine |
| Kosm. teh. Raket. vooruž. 2018 (1); 53-57 |
| Language: Russian |
|
Annotation:
The paper presents the variation of parameters of gas-vapor mixture of hypergolic rocket propellant components in a filling tank in the process of rocket propellant components filling into it with “closed drainage” depending on tank filing coefficient and initial parameters of environment in the tank.
|
