NASA Technical Note

NASA Technical Note PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 784

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NASA Technical Note

NASA Technical Note PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 784

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Book Description


NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 504

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Determination of Azimuth Angle at Burnout for Placing a Satellite Over a Selected Earth Position

Determination of Azimuth Angle at Burnout for Placing a Satellite Over a Selected Earth Position PDF Author: T. H. Skopinski
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 42

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 428

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NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32

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A Unified Form of Lambert's Theorem

A Unified Form of Lambert's Theorem PDF Author: E. R. Lancaster
Publisher:
ISBN:
Category : Orbital rendezvous (Space flight)
Languages : en
Pages : 28

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Chronological Catalog of Reported Lunar Events

Chronological Catalog of Reported Lunar Events PDF Author: Barbara M. Middlehurst
Publisher:
ISBN:
Category : Moon
Languages : en
Pages : 66

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Book Description
Chronological catalog of reported lunar events or temperature changes on moon recorded between 1540 and 1967.

Modern Engineering for Design of Liquid-Propellant Rocket Engines

Modern Engineering for Design of Liquid-Propellant Rocket Engines PDF Author: Dieter K. Huzel
Publisher: AIAA
ISBN: 9781600864001
Category : Liquid propellant rocket engines
Languages : en
Pages : 452

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Simplified Method for Determination of Critical Height of Distributed Roughness for Boundary-layer Transition at Mach Numbers from 0 to 5

Simplified Method for Determination of Critical Height of Distributed Roughness for Boundary-layer Transition at Mach Numbers from 0 to 5 PDF Author: Albert L. Braslow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624

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The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 870

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