Accession Number:

AD0854199

Title:

Tactical Missile Launcher Feasibility Study. Book II.

Descriptive Note:

Final rept.

Corporate Author:

HONEYWELL INC HOPKINS MINN ORDNANCE DIV

Personal Author(s):

Report Date:

1968-01-01

Pagination or Media Count:

241.0

Abstract:

The document contains inertial load tables and air load tables relative to the development and the results of a study of the feasibility of designing a standard tactical missile launcher which is capable of carrying and launching hypothetical stores, weighing from 500 to 3,000 pounds, from the F100, F101, F104 and F105 aircraft.

Subject Categories:

  • Attack and Fighter Aircraft
  • Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE