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- Preliminary Study of Aircraft Braking System with Emphasis on Fail-Safe Technology
- The Design of the GNC of the Re-Entry Module of Space Rider
- CRREL Report 93-14
- Comparison of Various Parachute Deployment Systems for Full Rocket Recovery of Sounding Rockets
- Northwest Indian College Space Center USLI Flight Readiness Review
- Incorporating the SJU-17A Naval Aircrew Common Ejection Seat in the EA-6B Aircraft
- Development and Testing of the Orion CEV Parachute Assembly System (CPAS)
- PIGEON Precision Integrated Geographical Navigation
- Eads Casa Cn-235
- ENRE 655 Class Project
- The Long Reach of the Stratojet
- Design, Analysis, and Test of a High-Powered Model Rocket
- 2020-2021 Launch 2 Learn Introductory Rocket Workshop
- Flight Readiness Review March 26, 2007
- Technical Memorandum
- Entry, Descent, and Landing Operations Analysis for the Genesis Entry Capsule
- Design, Development and Flight Performances of Deceleration System
- (CPAS) Generation I Pilot and Drogue Development Test Results
- Collection and Analysis of Dynamic Data with an Instrumented Aluminum High Power Rocket
- Oregon State University
- An Overview of the Guided Parafoil System Derived from X-38 Experience
- Tailoring a Parachute Recovery System for Commercial Space; the Commercial Crew Development II Parachute Recovery System for the CST-100 Space Capsule
- United States Patent (19) 11 Patent Number: 5,836,544 Gentile (45) Date of Patent: Nov
- CDR Presentation Slides (PDF, 927
- O At::Ithattor.EYS June 11, 1963 M
- University of Evansville Student Launch
- Design of a Windspeed Monitoring System for Autonomously-Guided Cargo
- Ram-Air Parachute Training Guide
- Noctua Technical Documentation
- SUMMARY of the ORBITER MECHANICAL SYSTEMS by John
- Parachutes Are Needed to Get to a Safe Landing Speed of 20 Mph Or Less
- NUSPACE Scientific Payloads: Atmospheric-Measurement and Controlled-Descent Experiment
- Arcilitidealiorzey