Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant PDF full book. Access full book title Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant by Jerry L. Modisette. Download full books in PDF and EPUB format.

Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant

Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant PDF Author: Jerry L. Modisette
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 14

Book Description

Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant

Preliminary Investigation of Lithium Hydride as a High-temperature Internal Coolant PDF Author: Jerry L. Modisette
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 14

Book Description

Qualitative Measurements of the Effective Heats of Ablation of Several Materials in Supersonic Air Jets at Stagnation Temperatures Up to 11,000° F

Qualitative Measurements of the Effective Heats of Ablation of Several Materials in Supersonic Air Jets at Stagnation Temperatures Up to 11,000° F PDF Author: Bernard Rashis
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 32

Book Description
Abstract: The ablation rates and effective heats of ablation were determined for a number of materials in supersonic ceramic-heated and electric-arc-powered air jets at stagnation temperatures ranging from 2,000° F to 11,000° F. The results indicated that the effective heats of ablation were from 7 to 40 times greater than the heat-absorption capacity of copper and increased with increasing aerodynamic heat flux. In addition, the results indicated that for the materials having phenolic-resin binders, the effective heats of ablation decreased with increasing resin content.

Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description

Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448

Book Description

A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

Book Description

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878

Book Description

Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1284

Book Description

NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 464

Book Description

Cumulative Title Index to United States Public Documents, 1789-1976

Cumulative Title Index to United States Public Documents, 1789-1976 PDF Author: Daniel W. Lester
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 774

Book Description

Preliminary Survey of Possible Cooling Methods for Hypersonic Aircraft

Preliminary Survey of Possible Cooling Methods for Hypersonic Aircraft PDF Author: Jack B. Esgar
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

Book Description
Abstract: Many methods of cooling the structure of an aircraft capable of flight speeds up to 18,000 feet per second were studied. Water and hydrogen stored in the liquid state appear very promising as both coolants and heat sinks. The storage and circulation of hydrogen throughout the aircraft need not be a hazard. Cooling the outer skin of the aircraft in high-equilibrium-temperature regions could probably be avoided by using a material such as silicon carbide. The internal structure could be cooled by use of a thin layer of balsa wood saturated with water. In this way tanks for storage of coolant would be avoided.
➤