Human Mars mission design study utilizing the adaptive deployable entry and placement technology

Engineering

• Design 100%
• Constraints 66%
• Ground Rule 33%
• Design Environment 33%
• Subsystems 33%
• Landing System 33%
• Heat Shield 33%
• Functional Requirement 33%
• Performance Parameter 33%
• Technical Challenge 33%
• Design Constraint 33%
• Determines 33%
• Performance 33%
• Models 33%
• Planning 33%
• Requirements 33%
• Architecture 33%

Computer Science

• Design 100%
• Risk Mitigation 66%
• Technical Challenge 33%
• Functional Requirement 33%
• Mitigation Activity 33%
• Key Requirement 33%
• Design Constraint 33%
• Performance Parameter 33%
• Classes 33%
• Models 33%