PARACHUTE FOR SEPARABLE NOSE CONE OF ROCKET PROJECTILE

FIELD: rocketry. SUBSTANCE: proposed parachute has round fabric canopy, lines and stabilizing ring which is provided with riffle band laid in circular link which is secured on stabilizing ring at distance of 0.2 to 0.5 of width of ring from its inlet hole. Length of band is calculated taking into ac...

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Bibliographische Detailangaben
Hauptverfasser:	KALJUZHNYJ G.V, KADYKOV V.M, SEMILET V.V, BAZARNYJ A.N, ROMANOVTSEV B.M, PLOTNIKOV A.E, BATOV A.G
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: rocketry. SUBSTANCE: proposed parachute has round fabric canopy, lines and stabilizing ring which is provided with riffle band laid in circular link which is secured on stabilizing ring at distance of 0.2 to 0.5 of width of ring from its inlet hole. Length of band is calculated taking into account diameter of inlet hole of stabilizing ring of unreefed parachute, drag coefficients both of reefed and unreefed parachutes and diameter of canopy deployment. Riffle band is made from caprone tape. EFFECT: enhanced reliability. 2 cl, 3 dwg