EXPERIMENTAL METHODS OF SOLID ROCKET PROPELLANT CHARACTERIZATION

The process of designing a solid-propellant rocket engine is a complex problem. Usually, it is solved by an iterative method, in which the initial data are gradually refined using experimental studies. With a sufficient statistical database, the problem is somewhat simplified because use can be made...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Datum:2026
1. Verfasser: VASYLIV, S. S.
Format: Artikel
Veröffentlicht: текст 3 2026
Online Zugang:https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/170
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Назва журналу:Technical Mechanics

Institution

Technical Mechanics