Normal view MARC view ISBD view

EFFECTS OF TARGET AND MISSILE CHARACTERISTICS ON THEORETICAL MINIMUM MISS DISTANCE FOR A BEAM-RIDER GUIDANCE SYSTEM IN THE PRESENCE OF NOISE

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1959Description: 32.DDC classification: NASA | MEMO 2-12-59A -

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA MEMO 2-12-59A - (Browse shelf)	Not for loan		TR7520

Total holds: 0

Previous								Next
Previous	NASA MEMO 1-8-59L - WIND-TUNNEL INVESTIGATION OF SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A TILTABLE-WING VERTICAL-TAKE-OFF-AND-LANDING SUPERSONIC BOMBER CONFIGURATION INCLUDING TURBOJET POWER EFFECTS	NASA MEMO 1-9-59L - HYDRODYNAMIC IMPACT-LOAD ALLEVIATION WITH A PENETRATING HYDRO-SKI	NASA MEMO 2-11-59E EFFECT OF STATOR AND ROTOR ASPECT RATIO ON TRANSONIC-TURBINE PERFORMANCE	NASA MEMO 2-12-59A - EFFECTS OF TARGET AND MISSILE CHARACTERISTICS ON THEORETICAL MINIMUM MISS DISTANCE FOR A BEAM-RIDER GUIDANCE SYSTEM IN THE PRESENCE OF NOISE	NASA MEMO 2-13-59A - SYNTHESIS OF OPTIMUM HOMING MISSILE GUIDANCE SYSTEMS WITH STATISTICAL INPUTS	NASA MEMO 2-13-59E EXEPERIMENTAL EVALUATION OF CERMET TURBINE STATOR BLADES FOR USE AT ELEVATED GAS TEMPERATURES.	NASA MEMO 2-16-59L - EFFECT OF ADSORBED NITROGEN ON THE THERMIONIC EMISSION FROM LANTHANUM HEXABORIDE	Next

Bound With Nasa Memo 2-3-59a-2-27-59a

There are no comments for this item.

PKK Library