Inverse venting problem for estimation of the discharge coefficient in a satellite launch vehicle
Abstract The pressure variation inside the heat shield of a satellite launch vehicle during ascent flight through the atmosphere induces structure load. If the depressurization of air is not rapid or appropriate, excessive pressure loading can cause structural failure of the heat shield or malfuncti...
Gespeichert in:
| Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2003-01, Vol.217 (6), p.277-281 |
|---|---|
| 1. Verfasser: | |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!