DEVELOPMENT TESTING OF THE L-1011 INDEPENDENT LANDING MONITORHOLLIDAY G; GORHAM JA.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1592-1605; BIBL. 2 REF.Serial Issue

INSTRUMENT LANDING SYSTEMS = SYSTEMES D'ATTERRISSAGESANDERS LL; FRITCH VJ JR.1973; I.E.E.E. TRANS. COMMUNIC.; U.S.A.; DA. 1973; VOL. 21; NO 5; PP. 435-454; BIBL. 63 REF.Serial Issue

A CASE HISTORY REPORT ON CARRIER LANDING SYSTEM. BURN. IN SOLVES RELIABILITY PROBLEMWOLFORD RE; CURRY C.1971; EVAL. ENGNG; U.S.A.; DA. 1971; VOL. 10; NO 5; PP. 16-19Serial Issue

ALLWETTERBETRIEB NACH KATEGORIE III UND/ODER ENTNEBELUNG = ATTERRISSAGE TOUT TEMPS EN CATEGORIE III ET/OU DISPERSION DU BROUILLARDCASTELL WD.1973; INTERNATION. VERKEHRSWES.; DTSCH.; DA. 1973; VOL. 25; NO 1; PP. 25-27; ABS. ANGLSerial Issue

HUMAN FACTORS IN LOW WEATHER OPERATION OF TRANSPORT AIRCRAFT = FACTEURS HUMAINS DANS LA MISE EN OEUVRE D'AVIONS DE TRANSPORT PAR MAUVAIS TEMPSWILSON JW.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 20.1-20.5; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

ANALYSIS OF LEGGED LANDERS FOR THE SURVIVABLE SOFT LANDING OF INSTRUMENT PAYLOADS = ANALYSE D'ATTERRISSEURS MUNIS DE JAMBES DESTINES A L'ATTERRISSAGE EN DOUCEUR ET SANS DOMMAGE DE CHARGES UTILES CONSTITUEES D'INSTRUMENTSLAURENSON RM; MELLIERE RA; MCGEHEE JR et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 208-214; BIBL. 6 REF.Serial Issue

METHODES DE CLASSIFICATION DES SYSTEMES NON LINEAIRES DES TRAINS D'ATTERRISSAGE D'AVIONSPRINC J.1972; STROJN. CAS.; CESKOSL.; DA. 1972; VOL. 23; NO 6; PP. 592-610; ABS. RUSSE ANGL.; BIBL. 12 REF.Serial Issue

LE SYSTEME SYDACPRESLES M.1973; NAVIGATION; FR.; DA. 1973; VOL. 21; NO 82; PP. 165-174Serial Issue

A SYSTEM FOR THE PRECISE CALIBRATION OF AIR NAVIGATIONAL RECEIVERSSORGER GU.1972; I.E.E.E. TRANS. INSTRUMENT. MEASUR.; U.S.A.; DA. 1972; VOL. 21; NO 4; PP. 519-527; BIBL. 7 REF.Serial Issue

MODERN LANDING IMPACT LOAD CALCULATIONS AND OLD FASHIONED REQUIREMENTSYFF J.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 31; PP. 1-9; BIBL. 7 REF.Conference Paper

THEORIE DES OSCILLATIONS D'UN AVIONLOBAS LG.1973; DOP. AKAD. NAUK U.R.S.R., A; S.S.S.R.; DA. 1973; VOL. 36; NO 3; PP. 258-262; ABS. ANGL. RUSSE; BIBL. 3 REF.Serial Issue

EXPERIMENTAL AND SIMULATION STUDY RESULTS OF A PLANETARY LANDING SITE SELECTION SYSTEM = RESULTATS D'UNE ETUDE EXPERIMENTALE ET PAR SIMULATION D'UN SYSTEME DE CHOIX D'UN SITE D'ATTERRISSAGE PLANETAIRESCHAPPELL RT; JOHNSON GR.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 277-280Serial Issue

TERRESTRIAL PROTOTYPE OF A LUNAR HOPPING TRANSPORTERPETERSON SH; MANNING JR.1972; IN: AM. SOC. MECH. ENG. WINTER ANNU. MEET.; NEW YORK, N.Y.; 1972; S.L.; A.S.M.E.; DA. 1972; VOL. AUT-7; PP. 1-4; BIBL. 7 REF.Conference Paper

ANTISKID AND MODERN AIRCRAFT = ANTIDERAPAGE ET AVIATION MODERNEHIRZEL EA.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 868; PP. 1-6Conference Paper

NON-STEADY-STATE THERMAL ANALYSIS OF A ROLLING AIRCRAFT TIRE = ANALYSE THERMIQUE EN REGIME NON STATIONNAIRE D'UN PNEUMATIQUE D'AVION EN ROULEMENTTRIVISONNO NM.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 871; PP. 1-24; BIBL. 2 REF.Conference Paper

KNEELING LANDING GEAR. THE C5 VARIABLE GEOMETRY DEVELOPMENT = TRAIN D'ATTERRISSAGE "AGENOUILLABLE". MISE AU POINT D'UNE GEOMETRIE VARIABLE POUR LE C-51973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 3; PP. 18-24 (3 P.)Serial Issue

SPACE SHUTTLE LANDING NAVIGATION USING DISTANCE MEASURING EQUIPMENT = NAVIGATION POUR L'ATTERRISSAGE D'UNE NAVETTE SPATIALE AVEC UTILISATION D'UN EQUIPEMENT POUR MESURER LES DISTANCES AVEC PRECISIONWIDNALL WS; MORTH HR.1972; NAVIGATION; U.S.A.; DA. 1972; VOL. 19; NO 4; PP. 377-389; BIBL. 16 REF.Serial Issue

AIRCRAFT LANDING SIMULATOR TESTS BRAKES AND TYRES SIMULTANEOUSLY1973; ELECTR. REV.; G.B.; DA. 1973; VOL. 192; NO 18; PP. 638-639Serial Issue

NEW DYNAMOMETER FACILITY1973; TECH AIR; G.B.; DA. 1973; VOL. 29; NO 4; PP. 5-7Serial Issue

REDUCTION OF ILS ERRORS CAUSED BY BUILDING REFLECTIONS = REDUCTION D'ERREURS ILS CAUSEES PAR DES REFLEXIONS SUR DES BATIMENTSGHOSE RN.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 167-171; BIBL. 2 REF.Serial Issue

AN OPTIMAL CONTROL APPROACH TO TERMINAL AREA AIR TRAFFIC CONTROL = UNE APPROCHE PAR LE CONTROLE OPTIMAL DU PROBLEME DE CONTROLE DE TRAFIC AERIEN EN AIRE TERMINALESCHMIDT DK; SWAIM RL.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 181-188; BIBL. 17 REF.Serial Issue

CANTILEVER AIRCRAFT TIRES. MORE THAN A BREAK FOR BRAKESWOODALL WR.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 870; PP. 1-9; BIBL. 1 REF.Conference Paper

PROBLEME DER INTEGRATION VON FLUGFUEHRUNGSSYSTEM BEI NEUEN ANFLUGVERFAHREN = PROBLEME DE L'INTEGRATION DES INSTRUMENTS DE VOL ET DES SYSTEMES DE PILOTAGE DANS LES NOUVEAUX DISPOSITIFS DE DECOLLAGE ET D'ATTERRISSAGESCHANZER G.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-20; H.T. 9; BIBL. 2 REF.Conference Paper

APPLICATION OF ENDFIRE ARRAYS AT CONTEMPORARY GLIDE-SLOPE PROBLEM SITESMCFARLAND RH.1981; IEEE TRANS. AEROSP. ELECTRON. SYST.; ISSN 0018-9251; USA; DA. 1981; VOL. 17; NO 2; PP. 261-270; BIBL. 18 REF.Article

ATTERRISSEURS D'AVION A COUSSIN D'AIRBRUNER G; LAURENT D.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 93-109; ABS. ANGL. ALLEM.; BIBL. 3 REF.Serial Issue