Click here to make tpub.com your Home Page

Page Title: Functional
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

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

 

Share on Google+Share on FacebookShare on LinkedInShare on TwitterShare on DiggShare on Stumble Upon
Back
Residual magnetism
Up
Thruster, Cartridge Actuated, M25A1 Assembly
Next
Load firing



img
MIL-T-60201C
p.
O-ring (2), P/N MS29513-212
q.
O-ring, P/N MS29513-214
r.
Cap Screw (2), P/N MS16998-9
4.3.4 Functional.
4.3.4.1 Ballistics. The test sample shall be rigidly supported so that the entire thrust is
borne by the thruster mounting points. The samples shall be tested within 10 minutes after removal
from the temperature conditioning chamber. When this time limit is exceeded, the sample units
shall be reconditioned at the original temperatures.
4.3.4.2 Temperature conditioning. Each assembled thruster shall be conditioned for not less
than 4 hours nor greater than 24 hours. When reconditioning thrusters at 65 F, all condensation
shall be removed from the exterior surfaces before returning the thruster to the conditioning
chamber.
4.4 Inspection of packaging. The sampling and inspection of the packaging, packing, and
container marking shall be in accordance with section 5.
5. PACKAGING
5.1 Packing and marking. Packing and marking shall be Level A or B, as specified by the
contracting activity (see 6.2). Level A shall be in accordance with Drawings 8797741 and 8797742.
Level B shall be in accordance with Drawings 8797741 and 9217579.
5.1.1 Lot numbers. Lot numbers shall be in accordance with MIL-STD-1168.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TPO 00-554-3103.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful but
is not mandatory.)
6.1 Intended use. The thruster assembly is used in conjunction with other propellant actuated
devices in Aircrew Emergency Escape Systems.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number, and revision letter of this specification
b. Issue of DODISS to be cited in the solicitation and, if required, the specific issue of
individual documents referenced (see 2.1.1 and 2.1.2)
11

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

Integrated Publishing, Inc.
9438 US Hwy 19N #311 Port Richey, FL 34668

Phone For Parts Inquiries: (727) 755-3260
Google +