STAGE OF ROCKET OF MULTIPLE USE

The utility model relates to rocket-space area. Stage of rocket for multiple use has body with propulsion compartment, transition compartment made of rotary panels, flexible shell in toroidal form with draining valves and support surface, rotary supports and parachute system. To increase operation p...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	LYKHACHOV MYKHAILO VOLODMYROVYCH, MOKIN OLEKSANDR VASYLIOVYCH, TERESCHENKO VASYL OLEKSANDROVYCH, SHAPOVALOV ANATOLII NYKYFOROVYCH, KUZEVANOV ARNOLD ARKADIIOVYCH, MOKIN ANDRII OLEKSANDROVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The utility model relates to rocket-space area. Stage of rocket for multiple use has body with propulsion compartment, transition compartment made of rotary panels, flexible shell in toroidal form with draining valves and support surface, rotary supports and parachute system. To increase operation properties support surface of flexible shell in working position is placed relative to long axis of the stage at angle value of which is chosen from condition that its sum with angle of stability of stage is smaller than right angle.