MIL-D-23660 Revision A:1965
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
DATA, TECHNICAL FOR ROCKET MOTORS
Available format(s)
PDF
Withdrawn date
28-08-1996
Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Details provisions for technical data to be prepared during the development program of rocket motors
| Committee |
FSC 1336
|
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-I-82787 Base Document:1990 | IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
| MIL-D-8684 Revision B:1959 | DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
| MIL-I-82826 Base Document:1985 | IGNITER ASSEMBLY |
| MIL-R-23139 Revision B:1965 | ROCKET MOTORS, SURFACE LAUNCHED, DEVELOPMENT AND QUALIFICATION REQUIREMENTS FOR |
| MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MIL-R-23139 Revision B:1965 | ROCKET MOTORS, SURFACE LAUNCHED, DEVELOPMENT AND QUALIFICATION REQUIREMENTS FOR |
| MIL D 5480 : F | DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
| MIL-STD-414 Base Document:1957 | SAMPLING PROCEDURE AND TABLE FOR INSPECTION BY VARIABLES FOR PERCENT DEFECTIVE |
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