SOLID PROPELLANT ROCKET ENGINE (VERSIONS)

FIELD: engines and pumps. ^ SUBSTANCE: solid propellant rocket engine comprises vessel, igniter, arranged in front or back part of engine, multi-nozzle unit concealed in vessel and insert charge of solid rocket propellant arranged in vessel and armoured along side surface and end. Multi-nozzle unit...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: VLASOV SERGEJ JAKOVLEVICH, SHVYKIN JURIJ SERGEEVICH, MOLCHANOV VLADIMIR FEDOROVICH, ANDREEV VLADIMIR ANDREEVICH, ARMISHEVA NATAL'JA ALEKSANDROVNA, KOZ'JAKOV ALEKSEJ VASIL'EVICH, NESHEV SERGEJ SERGEEVICH, KISLITSYN ALEKSEJ ANATOL'EVICH, AMARANTOV GEORGIJ NIKOLAEVICH
Format: Patent
Sprache:eng ; rus
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!