Accession Number:

AD0295489

Title:

Investigation to Determine the Feasibility of Using Inflatable Balloon Type Drag Devices for Recovery Applications in the Transonic, Supersonic, and Hypersonic Flight Regime. Part 2. Mach 4 to Mach 10 Feasibility Investigation

Descriptive Note:

Technical documentary rept.

Corporate Author:

GOODYEAR AEROSPACE CORP AKRON OH

Personal Author(s):

Report Date:

1962-12-01

Pagination or Media Count:

194.0

Abstract:

Subject Categories:

  • Military Aircraft Operations
  • Spacecraft Trajectories and Reentry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE