Author: Paul R. Knott
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 272
Book Description
Acoustic and Aerodynamic Performance Investigation of Inverted Velocity Profile Connualar Plug Nozzles
Author: Paul R. Knott
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 272
Book Description
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 272
Book Description
Monthly Catalog of United States Government Publications
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 876
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 876
Book Description
Aerodynamic and Acoustic Investigation of Inverted Velocity Profile Coannular Exhaust Nozzle Models and Development of Aerodynamic and Acoustic Prediction Procedures
Author: Richard S. Larson
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 228
Book Description
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 228
Book Description
Abstracts of NASA-ASRDI Publications Relevant to Aerospace Safety Research
150 and 300 KW Lightweight Diesel Aircraft Engine Study
Author: Alex P. Brouwers
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 156
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 156
Book Description
A 1-megawatt Reactor Design for Brayton-cycle Space Power Application
Author: C. L. Whitmarsh
Publisher:
ISBN:
Category : Brayton cycle
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Brayton cycle
Languages : en
Pages : 36
Book Description
Analysis of Thermal-protection Systems for Space-vehicle Cryogenic-propellant Tanks
Author: George R. Smolak
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 100
Book Description
Analytical techniques are presented that permit the calculation of heat-transfer rates with various thermal-protection systems for liquid-cryogenic-propellant tanks subjected to on-board, solar, and planetary heat fluxes. The effectiveness of these protection systems in reducing propellant heating is shown both for ideal heat-transfer models and for a simplified hydrogen-oxygen terminal state used for typical Mars missions.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 100
Book Description
Analytical techniques are presented that permit the calculation of heat-transfer rates with various thermal-protection systems for liquid-cryogenic-propellant tanks subjected to on-board, solar, and planetary heat fluxes. The effectiveness of these protection systems in reducing propellant heating is shown both for ideal heat-transfer models and for a simplified hydrogen-oxygen terminal state used for typical Mars missions.
Application of Powder Metallurgy to an Advanced-temperature Nickel-base Alloy NASA-TRW VI-A
Author: John C. Freche
Publisher:
ISBN:
Category : Heat resistant alloys
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Heat resistant alloys
Languages : en
Pages : 28
Book Description
Analysis of Centaur Propellant Utilization Difference Bridge
Author: O. James Magrini
Publisher:
ISBN:
Category : Centaur rocket
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Centaur rocket
Languages : en
Pages : 52
Book Description