Accession Number:

ADA801185

Title:

A Study of Several Parameters Controlling the Trajectories of a Supersonic Antiaircraft Missile Powered with Solid- or Liquid-Fuel Rockets

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER

Report Date:

1947-04-24

Descriptive Note:

Research memo.

Pages:

0046

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

1.80MB