MIL-P-53028 Base Document:1983
Withdrawn
Withdrawn
PROPELLANT, ROCKET MOTOR: ROCKET, HIGH EXPLOSIVE, 345 MILLIMETER, X130 (NO S/S DOCUMENT)
Available format(s)
PDF
Language(s)
English
Published date
09-06-1983
Publisher
Withdrawn date
01-09-1990
US$20.00
Excluding Tax where applicable
Requirements for XM130 High Explosive, 345 mm Rocket motor propellant.
| DocumentType |
Standard
|
| Pages |
12
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification establishes the requirements for the formulation of one type of propellant for the rocket motor for the Rocket, High, Explosive, 345 Millimeter: XM 130, herein referred as the propellant.
| ASTM D 792 : 2013 : REDLINE | Standard Test Methods for Density and Specific Gravity (Relative Density) of Plastics by Displacement |
| TT-M-261 Revision D:1970 | Methyl Ethyl Ketone, Technical (S/S by ASTM-D740) |
| MIL F 23938 : A | FERRIC OXIDE |
| MIL-STD-286 Revision C:1991 | Propellants, Solid: Sampling, Examination and Testing |
Summarise
US$20.00
Excluding Tax where applicable