DESIGN OF MAXIMUM THRUST NOZZLES FOR NONEQUILIBRIUM CHEMICALLY REACTING FLOW.TAYLOR AA; HOFFMAN JD.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1299-1300; BIBL. 9 REF.Article

VARIATION DE LA POUSSEE SPECIFIQUE DE L'ECOULEMENT DE GAZ DUE A LA NON-UNIFORMITE DU CHAMP DES VITESSES DU COL D'UNE TUYEREALEMASOV VE; DANILOV YU M; OPREDELYAKOV VA et al.1974; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1974; VOL. 17; NO 3; PP. 111-114; BIBL. 4 REF.Article

ADVANCED PINTLE-CONTROLLED MOTOR WITH THRUST VECTOR CONTROLSAYLES DC; LEVINSKY CT.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2557-2564Serial Issue

THRUSTER CHARACTERIZATION USING A THRUST BALANCE = CARACTERISATION D'UN PROPULSEUR UTILISANT L'EQUILIBRAGE DE LA POUSSEEBAILEY AG.1972; REV. SCI. INSTRUM.; U.S.A.; DA. 1972; VOL. 43; NO 12; PP. 1773-1774; BIBL. 1 REF.Serial Issue

ON THE MAXIMUM THRUST OF SAILS BY SAILING CLOSE TO WINDSPARENBERG JA; WIERSMA AK.1976; J. SHIP RES.; U.S.A.; DA. 1976; VOL. 20; NO 2; PP. 98-106; BIBL. 7REF.Article

THRUST STAND FOR EVALUATION OF THRUST-VECTORING NOZZLE PERFORMANCE = INSTALLATION DE MESURE DE POUSSEE POUR L'EVALUATION DES PERFORMANCES DE POUSSEE DE TUYERESESKER DW; SEDRICK AV.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-6; BIBL. 4 REF.Conference Paper

OPTIMAL LOW-THRUST TAKEOFF FROM AN ORBIT ABOUT AN OBLATE PLANET.JACOBSON RA; POWERS WF.1977; CELEST. MECH.; NETHERL.; DA. 1977; VOL. 15; NO 2; PP. 161-189; BIBL. 11 REF.Article

PROP-FAN. A HIGH THRUST, LOW NOISE PROPULSORROSEN G.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1654-1664; BIBL. 12 REF.Serial Issue

SECOND ORDER EFFECTS IN FLUIDMAGNETIC BUOYANCY.CURTIS RA.1974; APPL. SCI. RES.; NETHERL.; DA. 1974; VOL. 29; NO 5; PP. 342-350; BIBL. 3 REF.Article

A PROPULSION SYSTEM FOR ORBIT-TO-ORBIT SHUTTLEWELLS WW; LAMONT EA.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2586-2597Serial Issue

AIR BUOYANCY EQUATIONS FOR SINGLE-PAN BALANCES.WINWARD MR; WOOLLEY EM; BUTLER EA et al.1977; ANAL. CHEM.; U.S.A.; DA. 1977; VOL. 49; NO 13; PP. 2126-2128; BIBL. 2 REF.Article

EVALUATION DES CARACTERISTIQUES DE POUSSEE D'UNE TUYERE EJECTRICEDENISOV IN.1975; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1975; VOL. 18; NO 3; PP. 40-45; BIBL. 7 REF.Article

ETUDE THEORIQUE DES TUYERES CONVERGENTESDENISOV IN.1974; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1974; VOL. 17; NO 3; PP. 49-55; BIBL. 10 REF.Article

DIRECT THRUST MEASUREMENTS AND BEAM DIAGNOSTICS ON AN 18-CM KAUFMAN ION THRUSTERJUNGE HJ; SPRENGEL UW.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 101-105; BIBL. 6 REF.Serial Issue

TARGET-TYPE THRUST REVERSER NOISE = BRUIT PROVENANT D'INVERSEURS DE POUSSEE DE TYPE A CIBLESTONE JR; GUTIERREZ OA.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 283-288; BIBL. 5 REF.Serial Issue

PERFORMANCE OF A CASCADE THRUST REVERSER FOR SHORT-HAUL APPLICATIONS.DIETRICH DA; GUTIERREZ OA.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 3; PP. 185-191; BIBL. 9 REF.Article

CALCUL DES PERFORMANCES D'UNE TUYERE PROPULSIVE CONVERGENTE. COMPARAISON AVEC L'EXPERIENCE.FENAIN M; DUTOUQUET L; SOLIGNAC JL et al.1974; RECH. AEROSPAT.; FR.; DA. 1974; NO 5; PP. 261-276; ABS. ANGL.; BIBL. 8 REF.Article

STUDIES OF LEADING-EDGE THUST PHENOMENACARLSON HW; MACK RJ.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 12; PP. 890-897; BIBL. 14 REF.Article

GENERAL PRINCIPLES FOR THE AERODYNAMIC DESIGN OF SOLID ROCKET NOZZLES.JACQUES LJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1338; PP. 1-8; BIBL. 17 REF.Conference Paper

CONSIDERATIONS SUR LA STABILITE DES FLOTTEURS. I.DUPONT P; PLANEIX JM.1975; NAV. PORTS CHANTIERS; FR.; DA. 1975; NO 304; PP. 610-618; ABS. ANGLArticle

A SIMPLE ESTIMATE OF THE EFFECT OF EJECTOR LENGTH ON THRUST AUGMENTATION = UNE ESTIMATION SIMPLE DE L'INFLUENCE DE LA LONGUEUR DE L'EJECTEUR SUR L'AUGMENTATION DE POUSSEEQUINN B.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 313-314; BIBL. 6 REF.Serial Issue

ERDDRUCKUMLAGERUNGEN BEI RUECKVERANKERTEN JRAEGERBOHLWAENDEN = REDISTRIBUTION DE LA PRESSION ACTIVE DU SOL, DANS LE CAS DE PAROIS DE MADRIERS ANCREES DANS LE SOLBRISKE R.1980; BAUTECHNIK, AUSG. B; ISSN 0340-5044; DEU; DA. 1980; VOL. 57; NO 10; PP. 343-349; BIBL. 17 REF.Article

INCLINED ACTUATOR-DISE THEORY.CHESTER DH.1975; ISRAEL J. TECHNOL.; ISRAEL; DA. 1975; VOL. 13; NO 4; PP. 253-263; BIBL. 14 REF.Article

PERFORMANCE EVALUATION METHODS FOR THE HIGH-BYPASS-RATIO TURBOFAN.BARTLETT CR; TURNER EE.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1206; PP. 1-8; BIBL. 7 REF.Conference Paper

TECHNIQUES FOR DETERMINING PROPULSION SYSTEM FORCES FOR ACCURATE HIGH SPEED VEHICLE DRAG MEASUREMENTS IN FLIGHT.ARNAIZ HH.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 964; PP. 1-13; BIBL. 6 REF.Conference Paper