Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability
Title | Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability PDF eBook |
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Pages | 30 |
Release | 1964 |
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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4
Title | Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 PDF eBook |
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Pages | 78 |
Release | 1963 |
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The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3
Title | The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3 PDF eBook |
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Pages | 38 |
Release | 1961 |
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THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92
Title | THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 PDF eBook |
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Pages | 68 |
Release | 1961 |
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Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings
Title | Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings PDF eBook |
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Pages | 52 |
Release | 1963 |
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Coming Home
Title | Coming Home PDF eBook |
Author | Roger D. Launius |
Publisher | Government Printing Office |
Pages | 346 |
Release | 2012 |
Genre | Aerospace engineering |
ISBN | 9780160910647 |
NOTE; NO FURTHER DISCOUNT ON THIS PRINT PRODUCT-- OVERSTOCK SALE -- Signficantly reduced list price The technologies for the reentry and recovery from space might change over time, but the challenge remains one of the most important and vexing in the rigorous efforts to bring spacecraft and their crews and cargo home successfully. Returning to Earth after a flight into space is a fundamental challenge, and contributions from the NASA Aeronautics Research Mission Directorate in aerodynamics, thermal protection, guidance and control, stability, propulsion, and landing systems have proven critical to the success of the human space flight and other space programs. Without this base of fundamental and applied research, the capability to fly into space would not exist. Other related products: NASA Historical Data Book, V. 7: NASA Launch Systems, Space Transportation/Human Spaceflight, and Space Science can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01309-4 Revolutionary Atmosphere: The Story of the Altitude Wind Tunnel and the Space Power Chambers can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01342-6 Spinoff: Innovative Partnerships Program 2009 can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01331-1 Spinoff 2010: NASA Technologies Benefit Society can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01343-4 Spinoff 2015: Technology Transfer Program can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01372-8 Aerospace, Astronomy & Space Exploration resources collection can be found here: https: //bookstore.gpo.gov/catalog/science-technology/aerospace-astronomy... Other products produced by the U.S. National Aeronautics and Space Administration (NASA) can be found here: https: //bookstore.gpo.gov/agency/550"
Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0
Title | Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0 PDF eBook |
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Pages | 76 |
Release | 1961 |
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