ROCKET

FIELD: rocketry, in particular, salvo-fire jet systems. ^ SUBSTANCE: the rocket has a nose cone, solid-propellant rocket engine, stabilizer unit. The rear edges of the stabilizers in the area of the root chord are positioned at a distance of 0.5 to 0.7 of the diameter of the nozzle exit section. The...

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Bibliographische Detailangaben
Hauptverfasser:	PETROV VALERIJ LEONIDOVICH, KOROLEVA NATAL'JA BORISOVNA, DENEZHKIN GENNADIJ ALEKSEEVICH, VAN'KOV VIKTOR TIMOFEEVICH, PETURKIN DMITRIJ MIKHAJLOVICH, MAKAROVETS NIKOLAJ ALEKSANDROVICH, KASHIRKIN ALEKSANDR ALEKSANDROVICH, SEMILET VIKTOR VASIL'EVICH, TREGUBOV VIKTOR IVANOVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
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Beschreibung
Zusammenfassung:	FIELD: rocketry, in particular, salvo-fire jet systems. ^ SUBSTANCE: the rocket has a nose cone, solid-propellant rocket engine, stabilizer unit. The rear edges of the stabilizers in the area of the root chord are positioned at a distance of 0.5 to 0.7 of the diameter of the nozzle exit section. The nozzle subsonic section is made with an angle of 15 to 25 deg. The thickness of the nozzle subsonic section heat-resisting coating makes up 1.2 to 4 of the nozzle supersonic section heat-resisting coating. ^ EFFECT: makes it possible to produce a rocket with an improved accuracy and closely grouped fire. ^ 2 dwg