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 Serial/Series Title: NACA Research Memorandums
 Collection: National Advisory Committee for Aeronautics Collection
Heat-Transfer and Pressure Measurements from a Flight Test of the Second 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 by 10 to the 6th Power

Heat-Transfer and Pressure Measurements from a Flight Test of the Second 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 by 10 to the 6th Power

Date: January 29, 1958
Creator: Graham, J. B., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the Kingfisher XAUM-2 Flying Torpedo in the Langley Full Scale Tunnel, Ted No. NACA DE 327

Investigation of the Kingfisher XAUM-2 Flying Torpedo in the Langley Full Scale Tunnel, Ted No. NACA DE 327

Date: October 6, 1949
Creator: Barnett, U. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Induction system characteristics and engine surge occurrence for two fighter-type airplanes

Induction system characteristics and engine surge occurrence for two fighter-type airplanes

Date: May 26, 1958
Creator: Bellman, D. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds

Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds

Date: December 11, 1950
Creator: Nelson, W. H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of a liquid-metal turbine-propeller cycle for propulsion of low-speed nuclear- powered aircraft

Analysis of a liquid-metal turbine-propeller cycle for propulsion of low-speed nuclear- powered aircraft

Date: May 27, 1952
Creator: Rom, F. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of the maneuvering performance of a monowing versus a cruciform missile

A comparison of the maneuvering performance of a monowing versus a cruciform missile

Date: June 1, 1955
Creator: Matthews, H. F.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of a nuclear-powered liquid-metal ducted-fan cycle

Analysis of a nuclear-powered liquid-metal ducted-fan cycle

Date: December 17, 1952
Creator: Rom, F. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Pressure measurements on an afterbody behind various blunt nose shapes at a Mach number of 2

Pressure measurements on an afterbody behind various blunt nose shapes at a Mach number of 2

Date: December 27, 1957
Creator: Speegle, K. C.
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department
Organophosphorus compounds in rocket-engine applications

Organophosphorus compounds in rocket-engine applications

Date: April 2, 1954
Creator: Hennings, G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Sodium Hydroxide Reactor - Effect of Reactor Variables on Criticality and Fuel- Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion

The Sodium Hydroxide Reactor - Effect of Reactor Variables on Criticality and Fuel- Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion

Date: February 10, 1953
Creator: Bogart, D.
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department