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

MLS: ON THE BEAM FOR '76 = MLS: PRET POUR 1976EDWARDS JW.1973; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 24-30; BIBL. 3 REF.Serial 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

VIBRATIONS OF AN EULER BEAM WITH A SYSTEM OF DISCRETE MASSES, SPRINGS AND DASHPOTS = VIBRATIONS D'UNE POUTRE D'EULER AVEC SYSTEME DE MASSES DISCRETES, RESSORTS ET AMORTISSEURSRAVAGHAN KS; SUNDARARAJAN V.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 190-192; BIBL. 6 REF.Serial Issue

EVOLUTION ET ASPECT ACTUEL DE LA NAVIGATION AERIENNEFOMBONNE P.1973; NAVIGATION; FR.; DA. 1973; VOL. 21; NO 82; PP. 208-219; BIBL. 1 P. 1/2Serial Issue

MANUAL LANDINGS IN FOG = ATTERRISSAGES MANUELS DANS LE BROUILLARDNEWBERY RR.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 17.1-17.19; BIBL. 4 REF.; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

SAFETY1973; IN: PROC. 1973 ANNU. RELIAB. MAINTAINABILITY SYMP.; PHILADELPHIA, PA.; 1973; NEW YORK, U.S.A.; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 391-409; BIBL. DISSEM.Conference Paper

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

TRAJECTOGRAPHIE DE DECOLLAGE ET D'ATTERRISSAGEKLOPFSTEIN A; LEFIEVRE C.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 32-43; ABS. ANGL. ALLEMSerial 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

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

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

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

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

DISPLAY FUER STEILLANDER = INDICATEUR POUR ATTERRISSAGE VERTICALBEYER R.1973; D.F.V.L.R.-NACHR.; DTSCH.; DA. 1973; NO 9; PP. 382-383Serial Issue

OPTIMIZATION OF COMMERCIAL TRANSPORT AIRPLANE STOPPING SYSTEMS = OPTIMISATION DES SYSTEMES D'ARRET DES AVIONS DE TRANSPORT COMMERCIAUXMEREDITH DB; HAINLINE BC.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 872; PP. 1-10; BIBL. 3 REF.Conference Paper

TIRE DEVELOPMENT BY DEDICATED INVOLVEMENTSAVIERS H.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 869; PP. 1-10Conference 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