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Nebula Public Library

The knowledge bank of ESA’s R&D programmes

Aerocapture demonstration mission

Programme
Preparation
Programme Reference
21-P-M-HRE-06-b
Prime Contractor
ArianeGroup
Start Date
End Date
Status
Closed
Country
France
Aerocapture demonstration mission
Description

The AERODEM is an ESA demonstration mission that will implement an aerocapture phase in order to provide an atmospheric ∆V instead of a standard chemical one for orbiting a SpaceCraft around Mars. The aerocapture technique currently studied relies on a discrete event drag modulation technique that modifies only once the aerocapture module ballistic coefficient by separating / retracting the heatshield. In the perspective of future large missions to Mars, the mission will have to collect and transmit to Earth technology flight measurements that will be necessary for the implementation of the single drag modulation aerocapture technique. A pre-phase A study has been conducted by a consortium led by ArianeGroup with Airbus Defense & Space – Madrid, RTech and Jehier-Hutchison as partners. Two configurations are considered for AERODEM:

  • The Standalone configuration
  • The Piggy-Back configuration
Application Domain
Exploration
Technology Domain
10 - Flight Dynamics and GNSS
18 - Fluid Dynamics
20 - Structures
04 - Space Systems Environments and Effects
08 - System Design & Verification
09 - Mission Operation and Ground Data Systems
Competence Domain
02 - Structures / Mechanisms / Materials / Thermal
06 - Life / Physical Science Payloads / Life Support / Robotics and Automation
07 - Propulsion, Space Transportation and Re-entry Vehicles
10 - Astrodynamics / Space Debris / Space Environment
Keywords
aerocapture
aerobreaking
Mars
Orbit insertion
athmospheric drag
Re-entry
Orbital capture
Initial TRL
TRL N/A
Target TRL
TRL N/A
Achieved TRL
TRL N/A
Public Document
Executive Summary