DEFINITION:
Aero-assist and atmospheric entry (AAE) systems are defined as the intra-atmospheric technologies that decelerate a spacecraft from hyperbolic arrival through the hypersonic phase of entry. The mission requirements range from high-speed entries of scientific probes at Venus and Saturn, to sample return capsules to Earth (Mars sample return being the most challenging), and human missions to Mars.
(Source: NASA TA9.1 except TA9.1.5 Instrument & Health Monitoring included into 1-B-3 and TA9.1.6 Entry Modelling and Simulation included into 1-G-2)
SUBDOMAINS:
- Ground Tracking Networks: Covers the deployment, operation and data collection for GNSS sensor stations, network management, data handling services.
- GNSS and Geodetic Data Processing: Models, algorithms, data monitoring, data quality assessment and delivery of services and products.
- MEO and LEO Precise Orbit Determination Algorithms: Orbit dynamics and related models, analytical and numerical algorithms, for real-time (ground) and non-real-time (onboard/ground) data processing, performance analysis.
- Geodetic Reference Frames: Satellite geodesy, standards, processing of different observations.
Browsing taxonomies
Upper level
Sections at this level
- 01 AOCS/GNC Sensors and Actuators
- 02 Control System Engineering including innovative techniques
- 03 Control Techniques and Tools
- 04 Flight Dynamics
- 05 Global Navigation Satellite Systems (GNSS)
- 06 Radio Navigation Systems / Subsystems
- 07 Aero-assist and atmospheric entry
- 08 Descent and Targeting
- 09 Landing
- 10 Vehicle for EDL