Conceptual Development of a Payload Thermal and Pressure Control System for a Small Payload Quick Return Vehicle

An autonomous HAHO (high altitude, high-opening) parafoil system design is presented as a solution to the final descent phase of an on-demand International Space Station (ISS) sample return concept. The system design is tailored to meet specific constraints defined by a larger study at NASA Ames Research Center, called SPQR (Small Payload Quick-Return). Building on previous work in small, autonomous parafoil systems development, a SPQRcompatible evolution of an existing advanced parafoil delivery system is designed, built, and test-flown deployed from unmanned air vehicles and high-altitude balloons. Results of the preliminary tests of the original and SPQR-compatible systems are presented, and applicability of the test article to actual spaceflight conditions is discussed.

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Conceptual Development of a Payload Thermal and Pressure Control System for a Small Payload Quick Return Vehicle

Cited by 2 publications

References 2 publications

Developing and Testing a Spacecraft Phase Change Material Container for Water Ice Using Resilient Compressible Foam

Developing and Testing a Spacecraft Phase Change Material Container for Water Ice Using Resilient Compressible Foam

On Development of Autonomous HAHO Parafoil System for Targeted Payload Return

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