Propulsion Systems, Aircrew Escape, Design Specification

Click here to make tpub.com your Home Page

Page Title: Propulsion Systems, Aircrew Escape, Design Specification

Click here for thousands of PDF manuals

Web
www.tpub.com

Information Categories

....

Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion

Propulsion Systems, Aircrew Escape, Design Specification

Propulsion Systems, Aircrew Escape, Design Specification
Issues of Documents
Issues of Documents -Cont.
Issues of Documents -Cont.
Issues of Documents -Cont.
Issues of Documents -Cont.
Item Definition and Program Phases
Table I. Program Phase/Test Relationship
Movement of Internal Components
Table II. Design and Construction Documents
Dimensions
Combustion Chamber
Igniters and Ignition Materials
Propellant Formulations
Chemical and Physical Propellant Characteristics
Propellant Surfaces
Inhibitor (Insulator) and Disbond
Safety Pins
Torque Requirements of Threaded Joints
Rain, Humidity, and Salt Spray
Ballistics
Rate of Rise of Acceleration
Explosive Classification
Component Compatibility Tests
Design Verification Test Sample
Table III. Design Verification Test Program
Service Release Test
Table IV. Service Release Test Program
Table IV. Service Release Test Program -Cont.
Table IV. Service Release Test Program -Cont.
Air Force Procurement
Radiographic Inspection
Health and Safety Criteria
Configuration Management
Configuration Control
Types of Service Release
Reduction of Test Quantities
Test Equipment and Facilities
Recording Instruments
Safety of Handling
Ignition Material
Closed Bomb
Ballistic Data
Fungus Resistance
Humidity Test
Figure 1. Temperature Cycling for Initial Temprature of -65 Degree F
Figure 2. Temperature Cycling for Initial Temperature of 165 Degree F
External Heat Test
Compatibiltiy Tests
Fluid Connection Marking
Explosive Classification
Palletized Loads
Ordering Data
Contract Data Requirements
Figure 3. Sample Data Card
Table VI. Contract Data Requirements
Table VI. Contract Data Requirements
Rocket Motor Ignition Time
Solid Ejecta
Rate of Pressurization
Submission of Drawings
Standardization Document Improvement Proposal

Propulsion Systems, Aircrew Escape, Design Specification

Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business