Skip to main content

Inflatable Systems for Aerocapture and Aerobraking

Programme Reference

19-D-S-OPS-02

Status

Closed

Country

Portugal

Start Date

2020

End Date

2021

Programme: Discovery Prime Contractor: Spin.Works

Description

This work has primarily focused on establishing scenarios where inflatable devices could be the most useful. Given that these missions rely on aerodynamic drag that results in (potentially significant) heating, the authors have sought to find solutions to minimize heat fluxes acting on the device surface, and especially keeping it within the limits of flexible/foldable TPS materials for the aerocapture scenario. A second key challenge has been to minimize the mass per unit area, given that the most important way in which an inflatable contributes to a lower heating is by having a large surface (ensuring aerodynamic braking occurs at a lower atmospheric density).

Application domain: Exploration

Technology Domain:
10 - Flight Dynamics and GNSS
18 - Fluid Dynamics
09 - Mission Operation and Ground Data Systems
05 - Space System Control
04 - Space Systems Environments and Effects
08 - System Design & Verification
Competence Domain:
02 - Structures / Mechanisms / Materials / Thermal
07 - Propulsion, Space Transportation and Re-entry Vehicles
10 - Astrodynamics / Space Debris / Space Environment
Initial TRL: TRL N/A Target TRL: TRL N/A Achieved TRL: TRL N/A

Public Document:

Executive Summary
PDF

Inflatable Systems for Aerocapture and Aerobraking