| 2.3.5-2-1 Ensure Field-of-View/Field-of-Regard (FOV/FOR) requirements for all hardware are considered in the vehicle configuration |
Phase B |
Phase C |
|
Ensure consideration for FOV/FOR needs is incorporated into the vehicle layout. The FOV over the entire FOR should be considered. Payloads, attitude sensor, antennas and other like items all have Field-of-View and Field-of-Regard requirements. At CDR, ensure FOV/FOR requirements for all hardware and mechanical envelopes are considered and incorporated into the ICD, and vehicle layout.
|
NA
|
NA
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
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| 2.3.5-2-2 Ensure that the design/layout provides accessibility to components, to facilitate installation, removal and rework |
Phase B |
Phase C |
|
Ensure design considers access to each avionics/box for replacement, and that the perturbation to nearby boxes and cables is considered in the design.
|
NA
|
NA
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-3 Ensure that the mechanical design/spacecraft layout satisfies thermal constraints |
Phase B |
Phase C |
|
Ensure analysis of radiator location.
|
NA
|
NA
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-4 PLACEHOLDER |
Phase B |
Phase C |
|
PLACEHOLDER
|
NA
|
NA
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-5 Ensure the stowed configuration satisfies MDI related requirements |
Phase B |
Phase C |
|
Ensure minimized need for and complexity of deployables.
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-6 Ensure that the mechanical layout provides an efficient structural load path |
Phase B |
Phase C |
|
PLACEHOLDER
|
NA
|
NA
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-7 Ensure that the mechanical layout considers alignment requirements |
Phase B |
Phase C |
|
PLACEHOLDER
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-8 Ensure that Critical Clearances are identified and tracked |
Phase B |
Phase C |
|
Ensure analysis of critical clearances.
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-9 Ensure that ground handling considerations have been considered in the design |
Phase B |
Phase C |
|
Ensure movement of the entire SV, or larger subassemblies considers handling/facility limitations. This can include clearance for handling carts, overhead crane (hook)/ceiling heights, as well as pass thru(s), doorways, and aisle limitations. All sites where the SV or major subassemblies will be processed (including, e.g., subcontractor facilities, or the payload processing facility) should be considered in the evaluation.
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-10 Ensure the design maintains adequate clearances for harness integration |
Phase B |
Phase C |
|
Ensure the design incorporates adequate space for harness routing, tie downs, acceptable minimum bend radius, and access to connectors.
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|
| 2.3.5-2-11 Ensure the design of all actuation, launch lock and hold devices provides adequate access |
Phase B |
Phase C |
|
Ensure access to various hold down, actuation, and launch lock devices for installation, torqueing, inspection and refurbishment. Ensure that adequate proper access to these components is maintained.
|
NA
|
Design Review Data Package
|
TOR-2006(8506)-4494, Space Systems Engineering Handbook, MDI Section
|