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"Large-Scale Wind-Tunnel Tests of descent Performance of an Airplane Model Wigh A Tilt Wing and Differential Propeller Thrust" (NASA Technical Note TN D-1857), 1964-10

 Item — Box: MC-019-002, Folder: 001.A.051
Identifier: 20060028

Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-1857, dated October 1964.

Scope: Preliminary NASA research report by Wallace H. Deckert, V. Robert Page and Stanley O. Dickinson of Ames Research Center, Moffett Field, Calif.

Contents: See title

Dates

  • Publication: 1964-10

Creator

Conditions Governing Access

This collection is open for research in the Archives & Special Collections reading room. Handling guidelines and use restrictions will be communicated and enforced by archives staff members.

Extent

1 Issue

Language of Materials

English

Folder Contents

Items in the same folder (ID #s): 20060025, 20060026, 20060027 & 20060028.

Format & Physical Description

Saddle-stapled 8.5” x 11” booklet with tan cardstock covers (40 pages plus 2 pages of tear-out order coupons plus covers). Includes black & white photographs, charts, graphs and drawings. Staples have been removed.

Publication Data

Published by the National Aeronautics and Space Administration (NASA), Washington, D.C., dated October 1964.

Preservation

Preservation Level 3.V. Recommend digitizing this document when practicable.

Source

Repository Details

Part of the The University of Alabama in Huntsville Archives & Special Collections Repository

Contact:
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523