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

SCHWIERIGKEITEN BEIM BAROMETRISCHEN AUSSCHLEUSEN VON FLUESSIGKEITEN AUS DEM VAKUUM MITTELS FALLROHREN = DIFFICULTES RENCONTREES AU COURS DE L'EVACUATION BAROMETRIQUE DE LIQUIDES D'UNE ENCEINTE SOUS VIDE A L'AIDE DE TUBES DE GRAVITELAMBRECHT H.1973; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1973; NO 10; PP. 1-27; BIBL. 3 REF.Serial Issue

P80 La nouvelle génération de moteurs à propergol solide pour le spatial = P80 The new generation of solid propellant engines for aerospacePASCAL, Ph.Journées scientifiques Paul Vieille. 2004, pp 157-168, isbn 2-9521621-0-7, 1Vol, 12 p.Conference Paper

Analysis of the orbital inclination of Tansei 3 rocket 1977-12BMOORE, P.Planetary and space science. 1984, Vol 32, Num 9, pp 1101-1109, issn 0032-0633Article

FULL CONTROL OF SOLID PROPELLANT ROCKETS BY SECONDARY INJECTION = CONTROLE COMPLET DE FUSEES A PROPERGOLS SOLIDES PAR INJECTION SECONDAIREZEIERMAN I; MANHEIMER TIMNAT Y.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 161-162; BIBL. BIBL. (2 REF.Serial Issue

STAR TRACKING THROUGH THE EXHAUST BEAM OF MERCURY BOMBARDMENT THRUSTERS = POURSUITE D'ETOILES AU TRAVERS DU FAISCEAU DE SORTIE DE PROPULSEURS A BOMBARDEMENT DE MERCUREMILDER NL; SOVEY JS.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 47-51; BIBL. 18 REF.Serial Issue

BUOYANCY EFFECT ON FUEL CONTAINMENT IN A GAS-CORE NUCLEAR ROCKET = EFFET DE FLOTTABILITE SUR L'EMMAGASINAGE DU COMBUSTIBLE DANS UNE FUSEE NUCLEAIRE A COEUR GAZEUXPUTRE HA.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 932-934; BIBL. 4 REF.Serial Issue

Die Erdrakete als Sonde = The earth rocket as a probeGUDEHUS, G.BMT. Baumaschine + Bautechnik. 1993, Num 3, pp 129-134, issn 0005-6693Article

La Chine, nouvelle puissance spatialeSOTTY, Christian.La Recherche (Imprimé). 2012, Num 469, pp 72-74, issn 0029-5671, 3 p.Article

Fra Leipzig til London or From Leipzig to London: a translation from the danishCLYENS, S; JOHNSON, W.International journal of impact engineering. 1995, Vol 16, Num 1, pp 171-184, issn 0734-743XArticle

DISHED ACCELERATION GRIDS ON A 30-CM ION THRUSTERRAWLIN VK; BANKS BA; BYERS DC et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 29-35; BIBL. 16 REF.Serial Issue

ION THRUSTER THERMAL CHARACTERISTICS AND PERFORMANCEWEN L; CROTTY JD; PAWLIK EV et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 35-41; BIBL. 12 REF.Serial Issue

MANOEUVRE OPTIMALE D'ATTERRISSAGE SUR UNE PLANETE PAR UN MOTEUR A POUSSEE LIMITEE AVEC ANGLE D'ENTREE DONNE DANS L'ATMOSPHERE PLANETAIREKLIMKO AS.1973; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1973; NO 1; PP. 94-105; ABS. ANGL.; BIBL. 5 REF.Serial Issue

ATTITUDES OF THE ANTARCTIC SOUNDING ROCKET VEHICLESTOHYAMA F; AOYAMA I.1978; MEM. NATION. INST. POLAR RES., SPEC. ISSUE; JPN; DA. 1978; NO 9; PP. 87-91Conference Paper

AIAA SOUNDING ROCKET TECHNOLOGY CONFERENCE. 4. PROCEEDINGS; BOSTON, MASS.; 1976.1976; ; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. (308P.); BIBL. DISSEM.Conference Paper

On the computation of ionization levels in rocket exhaust flamesCOUSINS, J. M; JENSEN, D. E.Combustion and flame. 1983, Vol 52, Num 2, pp 111-125, issn 0010-2180Article

Fireworks and firemasters of England, 1662-1856JOHNSON, W.International journal of mechanical sciences. 1994, Vol 36, Num 11, pp 1061-1067, issn 0020-7403Article

DYNAMIC RESPONSES OF SOLID ROCKETS DURING RAPID PRESSURE CHANGE = REPONSES DYNAMIQUES DE FUSEES A PROPERGOLS SOLIDES DURANT DES VARIATIONS RAPIDES DE PRESSIONTURK SL; BATTISTA RA; KUO KK et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 137-142; BIBL. 14 REF.Serial Issue

THE ELECTRICAL PROPULSION OF SPACE VEHICULESBRIGHT AW; MAKIN B.1973; CONTEMPOR. PHYS.; G.B.; DA. 1973; VOL. 14; NO 1; PP. 25-38; BIBL. 4 REF.Serial Issue

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

DEVELOPMENT OF THE ALGOL III SOLID ROCKET MOTOR FOR SCOUTFELIX BR; MCBRIDE NM.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2565-2575; BIBL. 5 REF.Serial Issue

MINIMUM SMOKE SOLID PROPELLANT ROCKET MOTORSEVANS GI.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1192; PP. 1-11; H.T. 4Conference Paper

L'espace, crise actuelle = Space, actual crisisBIGNIER, M.Sciences (1969). 1996, Vol 96, Num 4, pp 28-32, issn 0151-0304Conference Paper

EXPERIMENTAL DETERMINATION OF THREE-DIMENSIONAL LIQUID ROCKET NOZZLE ADMITTANCESZINN BT; BELL WA; DANIEL BR et al.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 267-272; BIBL. 15 REF.Serial Issue

DETACHMENT OF THE OUTER SHOCK FROM UNDEREXPANDED ROCKET PLUMESPLOTKIN KJ; DRAPER JS.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1707-1709; BIBL. 17 REF.Serial Issue