Texas Attorney General Opinion: MS-220 (open access)

Texas Attorney General Opinion: MS-220

Letter opinion issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification; Constitutionality of Senate Bill 334, 54th Legislature, regulating practical nursing.
Date: June 7, 1955
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Safety experience -- Reactor and critical facilities (open access)

Safety experience -- Reactor and critical facilities

This report provides data as regards safety experience of the Hanford Production Reactors.
Date: June 7, 1955
Creator: Greager, O. H.
Object Type: Report
System: The UNT Digital Library
A Low-Pressure-Loss Short Afterburner for Sea-Level Thrust Augmentation (open access)

A Low-Pressure-Loss Short Afterburner for Sea-Level Thrust Augmentation

Memorandum presenting an investigation of the problems associated with the design of a low-pressure-loss, short afterburner for sea-level thrust augmentation in a static, sea-level test stand. Results regarding diffuser pressure losses, afterburner pressure losses, and afterburner performance are provided.
Date: June 7, 1955
Creator: Ciepluch, Carl C.; Velie, Wallace W. & Burley, Richard R.
Object Type: Report
System: The UNT Digital Library
A low-pressure-loss short afterburner for sea-level thrust augmentation (open access)

A low-pressure-loss short afterburner for sea-level thrust augmentation

Report presenting an investigation of the problems associated with the design of a low-pressure-loss, short afterburner for sea-level thrust augmentation in a static, sea-level test stand using the power section of a 5970-pound-thrust, axial-flow turbojet engine. The various portions of the afterburner and procedures used to test it are described. Results regarding diffuser pressure losses, afterburner pressure losses, and afterburner performance are provided.
Date: June 7, 1955
Creator: Ciepluch, Carl C.; Velie, Wallace W. & Burley, Richard R.
Object Type: Report
System: The UNT Digital Library
Redox Phase 3 capacity (open access)

Redox Phase 3 capacity

None
Date: June 7, 1955
Creator: McDonald, D.
Object Type: Report
System: The UNT Digital Library
Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane (open access)

Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane

"The importance of atomizing and mixing liquid oxygen and heptane was studied in a 200-pound-thrust rocket engine. Ten injector elements were used with both steel and transparent chambers. Characteristic velocity was measured over a range of mixture ratios. Combustion gas-flow and luminosity patterns within the chamber were obtained by photographic methods" (p. 1).
Date: June 7, 1955
Creator: Heidmann, M. F. & Auble, C. M.
Object Type: Report
System: The UNT Digital Library