| General Design and Verification | Former | Current |
|---|---|---|
| Test Requirements for Launch, Upper Stage, and Space Vehicles | MIL-STD-1540C | SMC-TR-04-171 |
| Test Method Standard for Environmental Engineering Considerations and Laboratory Tests | MIL-STD-810F | MIL-STD-810F |
| Software Development Standard for Space Systems | MIL-STD-498 | Aero. TOR-2004(3909)-3537, Rev. A |
| Test Requirements for Ground Equipment and Associated Computer Software Supporting Space Vehicles | MIL-STD-1833 | MIL-STD-1833 |
| Verification Requirements for Space Vehicles | — | Aero. TOR-2005(3901)-42432 |
| Domain-Specific Design and Verification | Former | Current |
| Electromagnetic Compatibility Requirements for Space Systems | MIL-STD-1541A | Aero. TOR-2005(8583)-1 |
| Electromagnetic Emissions and Susceptibility, Requirements for the Control of EMI | MIL-STD-461D | Aero. TOR-2005(8583)-1 |
| Wiring Harness, Space Vehicle, Design and Testing | DoD-W-8357A | DoD-W-8357A |
| Space Battery Standard | — | Aero. TOR-2004(8583)-5, Rev. 1 |
| Qualification and Quality Requirements for Space-Qualified Solar Panels | — | AIAA S-112-20051 |
| Electrical Power Systems, Direct Current, Space Vehicle Design Requirements | MIL-STD-1539A | Aero. TOR-2005(8583)-2 |
| Moving Mechanical Assemblies for Space and Launch Vehicles | MIL-A-83577C | AIAA S-114-20051 |
| Space Systems - Structures Design and Test Requirements | — | AIAA S-110-20051 |
| Space Systems - Flight Pressurized Systems | MIL-STD-1522A | Aero. TOR-2003(8583)-2896 |
| Space Systems - Metallic Pressure Vessels, Pressurized Structures, and Pressure Components | MIL-STD-1522A | AIAA S-080-19981 |
| Composite Overwrapped Pressure Vessels | MIL-STD-1522A | AIAA S-081-20001 |
| Solid Motor Case Design and Test Requirements | — | Aero. TOR-2003(8583)-2895, Rev. 1 |
| Criteria for Explosive Systems and Devices Used on Space Vehicles | DoD-E-83578A | AIAA S-113-20051 |
| Mass Properties Control for Satellites, Missiles, and Launch Vehicles | MIL-STD-1811 | Aero. TOR-2004(8583)-3970 |
| Part-Level Design and Verification | Former | Current |
| Qualification and Quality Standards for Space-Qualified Solar Cells | — | AIAA S-111-20051 |
| Electronic Parts, Materials, and Processes Control Program Used in Space Programs | MIL-STD-1547B | Aero. TOR-2004(3909)-3316, Rev. A |
| 1 These specifications have been converted to AIAA specifications based on Aerospace technical domain expertise submitted to AIAA technical committees via Aerospace TORs. 2 Not included on SMC compliance list. Included with NRO standards. |
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This table lists the specifications and standards that are being introduced or reintroduced into the national security space acquisition process that relate specifically to design and verification requirements. General design and verification specifications and standards typically apply to multiple levels of assembly and include some discussion of requirements oriented toward the integrated system-level architecture. Domain-specific standards are oriented toward environmental, functional, or hardware type testing and include requirements for batteries, solar panels, mechanisms, and structures. Part-level standards typically focus on space-related items. For details, see Aero. TOR-2003(8583)-2, Rev. 4, "Systems Engineering Revitalization Specifications and Standards Implementation Plan and Status."