NASA Procedural Requirements |
NPR 8079.1 Effective Date: June 27, 2023 Expiration Date: June 27, 2028 |
P.1 Purpose
P.2 Applicability
P.3 Authority
P.4 Applicable Documents and Forms
P.5 Measurement/Verification
P.6 Cancellation
1.1 Intent to Mitigate Spacecraft Collision Risk
1.2 Conjunction Analysis and Mitigation and the Project Life-Cycle
1.3 Conjunction Analysis and Mitigation Process Key Documents
1.4 Intra- and Interagency Coordination of Collision Avoidance
2.1 Office of the NASA Chief Engineer
2.2 Mission Directorate Associate Administrators
2.3 Project Managers
2.4 Conjunction Assessment Risk Analysis Program Manager
2.5 JSC Flight Operations Directorate Officers
2.6 SOMD Launch Services Office Manager
3.1 Overview
3.2 Orbital Collision Avoidance Plan
3.3 Conjunction Assessment Operations Implementation Agreement
4.1 Overview
4.2 Conjunction Assessment Step
4.3 Conjunction Risk Assessment Step
4.4 Conjunction Mitigation Step
5.1 Ephemeris Sharing
5.2 Maneuverable Spacecraft
5.3 Conjunction Mitigation
5.4 Post-Launch Deployments
5.5 Advanced Capabilities
Figure 1-1 Earth-Orbiting Collision Avoidance Process for a NASA-Owned or -Operated Spacecraft
Figure 1-2 Conjunction Assessment
Figure 1-3 Conjunction Risk Assessment
Figure 1-4 Conjunction Mitigation
Figure 3-1 Orbital Collision Avoidance Plan Flow
Figure 4-1 Conjunction Analysis and Mitigation Process Flowchart
Table 3-1 Example Conjunction Assessment Activities Throughout an NPR 7120.5 Project Life Cycle
Table 3-2 Example Conjunction Assessment Activities Throughout an NPR 7120.8 Project Life Cycle
Table 5-1 Ephemeris Specifications
Table C-1 NASA Spacecraft Conjunction Analysis and Collision Avoidance for Space Environment Protection Compliance Matrix
Table D-1. Planning Activities for Deployment Scenarios
Table D-2. Inputs, Analyses, and Context for OCAP Fields
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