SAE ARP1833B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Sealing Techniques for Missile Applications
Hardcopy , PDF
11-05-2023
English
15-01-2015
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. REFERENCES
3. ELASTOMERIC O-RING SEAL GUIDELINES
4. NOTES
Specifies the missile hydraulic and pneumatic component designer with information learned, tested and substantiated in correction of problems and failures experienced with seals that are subject to the unique requirements of missile static storage and subsequent dynamic operational conditions.
| DocumentType |
Standard
|
| Pages |
42
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
The purpose of this standard is to provide the missile hydraulic and pneumatic component designer with information learned, tested and substantiated in correction of problems and failures experienced with seals that are subject to the unique requirements of missile static storage and subsequent dynamic operational conditions.
| SAE AS4716B | Gland Design, O-ring and Other Elastomeric Seals |
| ISO 3601-2:2016 | Fluid power systems — O-rings — Part 2: Housing dimensions for general applications |
| SAE AIR1412C | Designing for Long Life with Elastomers |
| ASME Y14.5 : 2009 | DIMENSIONING AND TOLERANCING |
| SAE ARP1234B | Gland Design, Elastomeric O-Ring Seals, Static Axial, Without Back-Up Rings |
| SAE AIR786B | Elastomer Compatibility Considerations Relative to Elastomeric Sealant Selection |
| SAE AS 5857 : 2010 | GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS, STATIC APPLICATIONS |
| SAE AS6235A | Face Seal Gland Design, Static, O-ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications |
| SAE ARP1231A | Gland Design, Elastomeric O-Ring Seals, General Considerations |
| SAE AMS7379 | Rubber: Fluorocarbon Elastomer (FKM) 70 to 80 Hardness, Low Temperature Sealing Tg −40 °F (−40 °C) For Elastomeric Seals in Aircraft Engine Oil, Fuel and Hydraulics Systems |
| ISO 3601-3:2005 | Fluid power systems O-rings Part 3: Quality acceptance criteria |
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