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1801.
|
APOLLO EXPERIENCE REPORT - EARTH LANDING SYSTEM
by West,Robert B. Material type:  Book Description: 76.Publisher: Nasa, Washington, D.C. 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7437 -] (1).
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1802.
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APOLLO EXPERIENCE REPORT - RELIABILITY AND QUALITY ASSURANCE
by Sperber,K P. Material type: Book Description: 31.Publisher: Nasa, Washington, D.C. 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7438 -] (1).
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1803.
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APOLLO EXPERIENCE REPORT - SPACECRAFT STRUCTURAL WINDOWS
by Pigg,Orvis E | Weiss,Stanley P. Material type: Book Description: 18.Publisher: Nasa, Washington, D.C. 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7439 -] (1).
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1804.
|
FREE-FLIGHT INVESTIGATION OF THE DEPLOYMENT, DYNAMIC STABILITY, AND CONTROL CHARACTERISTICS OF A 1/12-SCALE DYNAMIC RADIO-CONTROLLED MODEL OF A LARGE BOOSTER AND PARAWING
by Burk,Jr.,Sanger M. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1932 -] (1).
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1805.
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EFFECT OF FABRICATION-TYPE SURFACE ROUGHNESS ON TRANSITION ON OGIVE-CYLINDER MODELS AT MACH NUMBERS OF 1.61 AND 2.01
by Howard,Paul W | Czarnecki,K R. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1933 -] (1).
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1806.
|
INVESTIGATION OF THE LANDING CHARACTERISTICS OF A REENTRY VEHICLE HAVING CANTED MULTIPLE-AIR-BAG LOAD-ALLEVIATION SYSTEM
by Stubbs,Sandy M | Mcgehee,John R. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1934 -] (1).
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1807.
|
LOADS INDUCED ON A FLAT PLATE AT A MACH NUMBER OF 4.5 WITH A SONIC OR SUPERSONIC JET EXHAUSTING NORMAL TO THE SURFACE
by Letko,William. Material type: Book Description: 24.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1935 -] (1).
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1808.
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TRAILBLAZER I REENTRY-BODY WIND-TUNNEL TESTS AT A MACH NUMBER OF 6.7 WITH THEORETICAL AERODYNAMICS AND A LIMITED DYNAMIC ANALYSIS
by Schippell,Herbert R. Material type: Book Description: 24.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1936 -] (1).
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1809.
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LOW-SPEED INVESTIGATION OF CABLE TENSION AND AERODYNAMIC CHARACTERISTICS OF A PARAWING AND SPACECRAFT COMBINATION
by Sleeman,Jr.,William C. Material type: Book Description: 59.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1937 -] (1).
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1810.
|
TRAJECTORY ANALYSIS OF A VARIABLE-DRAG PAYLOAD EJECTED FROM A VEHICLE IN A LOW EARTH ORBIT
by Reid,Richard | Middleton,Savid B. Material type: Book Description: 28.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1938 -] (1).
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1811.
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ANALYSIS OF THE LUNAR RETURN MISSION
by Gapcynski,John P | Tolson,Robert H. Material type: Book Description: 29.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1939 -] (1).
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1812.
|
INVESTIGATION OF THE NATURAL FREQUENCIES AND MODE SHAPES OF DOUBLE CONICAL SANDWICH DISKS
by Thompson,Jr.,William M | Clary,Robert R. Material type: Book Description: 25.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1940 -] (1).
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1813.
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EFFECT OF LEADING-EDGE SWEEP AND SURFACE INCLINATION ON THE HYPERSONIC FLOW FIELD OVER A BLUNT FLAT PLATE
by Creager,Marcus O. Material type: Book Description: 45.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1814.
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EFFECT OF LOWER SURFACE SPOILERS ON THE TRANSONIC TRIM CHANGE OF A WIND-TUNNEL MODEL OF A FIGHTER AIRPLANE HAVING A MODIFIED DELTA WING
by Robinson, Robert C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 50p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1815.
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EFFCET OF LARGE WING-TIP MASSES ON OSCILLATORY STABILITY OF WING BENDING COUPLED WITH AIRPLANE PITCH
by Higdon,Donald T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 32p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1816.
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EXPLORATORY INVESTIGATION OF THE EFFECTS OF BOUNDARY-LAYER CONTROL ON THE PRESSURE-RECOVERY CHARACTERISTICS OF A CIRCULAR INTERNAL-CONTRACTION INLET WITH TRANSLATING CENTERBODY AT MACH NUMBERS OF 2.0
by Martin, Norman J. Material type: Book Description: 44p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1817.
|
LANDING LOADS AND DYNAMICS OF THE X-15 AIRPLANE
by Mckay,James M | Kordes,Eldon E. Material type: Book Description: 16.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TMX-639 -] (1).
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1818.
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EXPERIMENTAL INVASTIGATION OF A DISK-SHAPED REENTRY CONFIGURATION AT TRANSONIC AND LOW SUPERSONIC SPEEDS
by Lazzeronl,Frank A. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TMX-652 -] (1).
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1819.
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INVESTIGATION OF LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 0.34-SCALE FREE-FLYING MODEL OF A MODIFIED HALF-CONE REENTRY VEHICLE
by Hassell,James L | Ware,George M. Material type: Book Description: 41.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TMX-665 -] (1).
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1820.
|
WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC AND STRUCTURAL-DEFLECTION CHARACTERISTICS OF AN INFLATABLE AIRPLANE
by Mclemore,H. Clyde. Material type: Book Description: 202.Publisher: Nasa, Washington, D.C. 1962Availability: No items available Damaged (1).
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