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

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

ROCKET NOZZLE DAMPING CHARACTERISTICS MEASURED USING DIFFERENT EXPERIMENTAL TECHNIQUES.JANARDAN BA; ZINN BT.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 442-444; BIBL. 7 REF.Article

COMBUSTION OF HIGHLY LOADED COMPOSITE PROPELLANTS: STUDY OF PRESSURE EXPONENTS.EPHRAIM COHEN NIR.1976; COMBUST. SCI. TECHNOL.; G.B.; DA. 1976; VOL. 14; NO 1-3; PP. 75-84; BIBL. 9 REF.Article

SPACECRAFT CHARGING DUE TO POSITIVE ION EMISSION: AN EXPERIMENTAL STUDYCOHEN HA; SHERMAN C; MULLEN EG et al.1979; GEOPHYS. RES. LETTERS; USA; DA. 1979; VOL. 6; NO 6; PP. 515-518; BIBL. 8 REF.Article

CONTROLE DES PROPULSEURS PAR HOLOGRAPHIE.SMIGIELSKI P; STIMPFLING A.1975; ISL-R-134-75; FR.; DA. 1975; PP. (100P.); ABS. ALLEM.; BIBL. 12 REF.Report

Investigation of liquid gun propellants : electrical ignition of LGP 1846KLINGENBERG, G; ROCKSTROH, H; KNAPTON, J. D et al.Propellants, explosives, pyrotechnics. 1990, Vol 15, Num 3, pp 103-114, issn 0721-3115, 12 p.Article

UTILIZATION OF A ROBOT SYSTEM ON THE SOLIT ROCKET BOASTER COMPONENTS FOR THE NASA SPACE SHUTTLE PROGRAMSWEET GK.1980; INTERNATIONAL SYMPOSIUM ON INDUSTRIAL ROBOTS. 10. INTERNATIONAL CONFERENCE ON ROBOT TECHNOLOGY. 5/1980/MILAN; GBR; KEMPSTON: IFS (PUBLICATIONS); DA. 1980; PP. 1-13Conference Paper

FOTOMETR RENTGENOWSKI DO RAKIETY GEOFIZYCZNEJWERTYKAL 5 = PHOTOMETRE A RAYONS X SOLAIREHLOND M.1978; POST. ASTR.; POL; DA. 1978; VOL. 26; NO 3; PP. 201-207; ABS. RUS/ENGArticle

EINIGE UNTERSUCHUNGEN AN FLUGKOERPERN MIT ZENTRALSTIFT ALS STEUERORGAN BEI HOHEN MACHZAHLEN. = QUELQUES ETUDES DE MISSILES AYANT UNE POINTE COMME ORGANE DE COMMANDE AUX MEMBRES DE MACH ELEVESWYBORNY W.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 3; PP. 1-30; ABS. ANGL.; BIBL. 7 REF.Serial Issue

ENERGIEVERLUSTE IN HOCHENERGETISCHEN RAKETENTRIEBWERKEN BEI SCHUBVARIATION. = PERTES D'ENERGIE DANS DES MOTEURS DE FUSEE A HAUTE ENERGIE AVEC VARIATION DE POUSSEESTERNFELD HJ.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 41; PP. 1-101; ABS. ANGL.; BIBL. 7 P. 1/2Serial Issue

PRESSURE DEPENDENCE OF HYBRID FUEL BURNING RATE.RASTOGI RP; DESH DEEPAK.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 988-990; BIBL. 12 REF.Article

MEASURED MOLECULAR ABSORPTIVITIES FOR A LASER THRUSTERFOWLER MC.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 8; PP. 1009-1014; BIBL. 16 REF.Article

THE FAR ULTRAVIOLET (1200-1900 A) SPECTRUM OF JUPITER OBTAINED WITH A ROCKET-BORNE MULTICHANNEL SPECTROMETER.GILES JW; MOOS HW; MCKINNEY WR et al.1976; J. GEOPHYS. RES.; U.S.A.; DA. 1976; VOL. 81; NO 34; PP. 5797-5806; BIBL. 49 REF.Article

DETERMINATION EXPERIMENTALE DES CARACTERISTIQUES DE LA PRECISION, RELATIVES AUX MESURES METEOROLOGIQUES PAR FUSEESLYSENKO EV; ROZENFEL'D S KH; SPERANSKIJ KE et al.1982; METEOROL. GIDROL.; ISSN 0130-2906; SUN; DA. 1982; NO 10; PP. 46-52; ABS. ENG; BIBL. 10 REF.Article

ESRANGE: A HIGH-LATITUDE ROCKET AND BALLOON RANGE MANAGED BY THE SWEDISH SPACE CORPORATION.LARSSON LH.1976; E.S.A. BULL.; FR.; DA. 1976; NO 7; PP. 74-76Article

AN EARTH SURVEY SYSTEM DESIGN USING THE KAPPA-8 ROCKETSALATUN AS.1979; PROC-INST. TEKNOL. BAUDUNG; ISSN 0522-2133; IDN; DA. 1979; VOL. 12; NO 3; 22 P.; ABS. IND; BIBL. 8 REF.Serial Issue

EIN PIRANI-MANOMETER FUER METEOROLOGISCHE RAKETENSOUDEN. = UN MANOMETRE DE PIRANI POUR LES FUSEES-SONDES METEOROLOGIQUESASSENG E.1977; Z. METEOROL.; DTSCH.; DA. 1977; VOL. 27; NO 3; PP. 160-174; ABS. ANGL.; BIBL. 6 REF.Article

A DIRECTLY READING SLANT RANGE SYSTEM.FRIEDRICH M; URBAN A.1977; SPACE SCI. INSTRUMENT.; NLD; DA. 1977; VOL. 3; NO 4; PP. 449-453; BIBL. 3 REF.Article

MINIMUM-FUEL ROCKET TRAJECTOIRES INVOLVING INTERMEDIATE-THRUST ARCS.BREAKWELL JV; DIXON JF.1975; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1975; VOL. 17; NO 5-6; PP. 465-479; BIBL. 10 REF.Article

Steady-state high pressure LOx/H2 rocket engine combustionSMITH, Joshua J; SCHNEIDER, Gerald; SUSLOV, Dmitry et al.Aerospace science and technology. 2007, Vol 11, Num 1, pp 39-47, issn 1270-9638, 9 p.Conference Paper

PropellantsKayaku Gakkaishi. 1996, Vol 57, Num 4, issn 1340-2781, 38 p.Serial Issue

VORAUSSICHTLICHER ALUMINIUMBEDARF IN DER WELTRAUMTECHNOLOGIE = FORECAST DEMAND FOR ALUMINIUM IN SPACE TECHNOLOGYKAINDL K.1982; ALUMINIUM (DUESSELD.); DEU; DA. 1982-05; VOL. 58; NO 5; PP. 285-286; BIBL. 13 REF.Article

LASER PROPULSIONWEISS RF; PIRRI AN; KEMP NH et al.1979; ASTRONAUT. AND AERONAUT.; USA; DA. 1979; VOL. 17; NO 3; PP. 50-58; BIBL. 30 REF.Article

0 KG: UN POIDS JUSQU'A PRESENT JAMAIS ATTEINT POUR UNE PIECE MOULEE EN ALLIAGE DE MAGNESIUM1977; FONDERIA ITAL.; ITAL.; DA. 1977; VOL. 26; NO 2; PP. 53Article