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SELF-ERECTING FLEXIBLE FOAM STRUCTURES FOR SPACE ANTENNAS.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 16.DDC classification: NASA | TN D-1610

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1610 (Browse shelf)	Not for loan		TR11982

Total holds: 0

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Previous	NASA TN D-1605 EXPLORATORY INVESTIGATION OF THE EFFECT OF A FORWARD-FACING JET ON THE BOW SHOCK OF A BLUENT BODY IN A MACH NUMBER 6 FREE STREAM.	NASA TN D-1606 AERODYNAMIC CHRACTERISTICS AT A MACH NUMBER OF 6.77 OF A 9 DEGREE CONE CONFIGURATION, WITH AND WITHOUT SPHERICAL AFTERBODIES,AT ANGLES OF ATTACK UP TO 180 DEGREE WITH VARIOUS DEGREES OF NOSE BLUNTING.	NASA TN D-1608 AN ANALYTICAL STUDY OF A SIMPLE ATTITUDE CONTROL SYSTEM FOR A FINNED VEHICLE.	NASA TN D-1610 SELF-ERECTING FLEXIBLE FOAM STRUCTURES FOR SPACE ANTENNAS.	NASA TN D-1612 PRESSURE DISTRIBUTIONS OVER THE FORWARD PORTION OF THE PROJECT FIRE SPACE-VEHICLE CONFIGURATION AT MACH NUMBER FROM 0.25 TO 0.60	NASA TN D-1613 POLOT-CONTROLLED SIMULATION OF RENDEZVOUS BETWEEN A SPACE CRAFT AND A COMMANDED MODULE HAVING LOW THRUST	NASA TN D-1614 EXPERIMENTAL INVESTIGATION OF THE DYNAMIC STABILITY STABILITY OF A TOWED PARAWING GLIDER MODEL	Next

Bound With Nasa Tn D-1601-1609.

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