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TB-9-1377-200 Propellant Actuated Devices Manual
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Table of Contents (cont)

TB 9-1377-200/TO 11P-1-14
TECHNICAL BULLETIN
DEPARTMENTS OF THE ARMY
No. No. 9-1377-200
AND THE AIR FORCE
TECHNICAL ORDER
No. 11P-1-4
WASHINGTON, D.C., 8 November 1965
PROPELLANT ACTUATED DEVICES
INTRODUCTION .....................................................................
Paragraph
Page
Purpose and scope ..................................................................
Reporting of bulletin improvements .........................................
References ..............................................................................
History .....................................................................................
Uses ........................................................................................
DESCRIPTION OF PROPELLANT ACTUATED DEVICES
General ...................................................................................
Gas-generating devices ...........................................................
Stroking devices ......................................................................
Special purpose devices ..........................................................
Systems ..................................................................................
BASIC DESIGN
General ...................................................................................
Motion or time functions ..........................................................
Load ........................................................................................
Weight and size (envelope) .....................................................
Environment ............................................................................
Heat loss .................................................................................
DESIGN TECHNIQUES
INTRODUCTION
General ...................................................................................
Design requirements................................................................
METHOD OF FIRST ORDER APPROXIMATIONS
General ...................................................................................
Stroke to separation ................................................................
Stroke time ..............................................................................
Peak pressure .........................................................................
Propellant charge weight .........................................................
Propellant web.........................................................................
Cartridge case volume.............................................................
Igniter charge ..........................................................................
DESIGN STRENGTH CALCULATIONS
General ...................................................................................
Safety factors ..........................................................................
Temperature effects ................................................................
Stresses ..................................................................................
Distortion-energy theory ..........................................................
Length of thread engagement ..................................................
DESIGN PROCEDURES
General ...................................................................................
Gas-generating devices ...........................................................
Stroking devices ......................................................................
Systems ..................................................................................
COMPONENT DESIGN
Cartridge .................................................................................
Body and chamber ..................................................................
Piston ......................................................................................
Firing mechanism ....................................................................
Locking mechanisms ...............................................................
Seals .......................................................................................
i

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