ASTEROID PROSPECTION EXPLORER (APEX) CUBESAT FOR … · APEX Science Asteroid Prospection Explorer...
Transcript of ASTEROID PROSPECTION EXPLORER (APEX) CUBESAT FOR … · APEX Science Asteroid Prospection Explorer...
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APEX Science
Asteroid Prospection Explorer (APEX) is a 6U CubeSat developed for Hera mission being part of ESA-NASA AIDA
(Asteroid Impact & Deflection Assessment) project. APEX features a unique set of instruments designed to provide a global
characterization of the Didymos system – target of the joint ESA-NASA Asteroid Impact and Deflection Assessment
(AIDA) mission. The instrument set includes ASPECT (Asteroid Spectral Imager), ACA (Asteroid Composition Analyzer),
and MAG (Magnetometer).
ASTEROID PROSPECTION EXPLORER (APEX) CUBESAT FOR HERA MISSIONT. Kohout1,2, Jan-Erik Wahlund3 Tatsuo Shimizu4, Tomi Kärkkäinen4, Daniel Štefl5 and APEX team
1. Faculty of Science, University of Helsinki, Finland ([email protected])
2. Institute of Geology, The Czech Academy of Sciences, Prague, Czech Republic
3. Swedish Institute of Space Physics (IRF), Upsalla, Sweden
4. Reaktor Space Lab, Espoo, Finland
5. Space Systems Czech, Prague, Czech Republic
Conclusions
APEX is a deep space CubeSat with a VIS-MIR hyperspectral imager, magnetometer, and secondary ion spectrometer.
Main science objectives are to characterize target surface, composition, and internal structure.
Acknowledgments
The project is done under ESA GSTP contract and is partly supported by Academy of Finland and ERC.
Scientific objectives
1. Map the global composition of the Didymos asteroids
→ Result: Mineral composition and homogeneity of the Didymos asteroid surface
→ Result: Elemental composition of the Didymos asteroid surface
→ Result: Constrain FeNi amount from induced component of the magnetic field
2. Determine the internal structure and evolution of the Didymos system
→ Result: Mineral and elemental composition differences between Didymos I and II
→ Result: Detection and origin of the magnetization of the Didymos asteroid material
→ Result: Size of building blocks of the Didymos asteroids inferred from their remanent
magnetic signature
3. Determine surface roughness or regolith grain size of the Didymos asteroids
→ Result: Surface particle size distribution and composition for Didymos I and II
4. Evaluate space weathering effects on Didymos II by comparing mature and freshly exposed
material
→ Result: Optical and possible elemental differences between mature and freshly exposed
material
5. Identify local shock effects on Didymos II caused by DART impact based on spectral
properties of crater interior
→ Result: Determine optical properties of the material within crater
→ Result: Determine elemental composition on surface, differences inside and outside the
crater
→ Result: Determine magnetic signature of the crater
6. Map global fallback ejecta on Didymos I and II
→ Result: Detailed global mapping of fallback ejecta on both Didymain and Didymoon
7. Characterize interaction of Didymos system with interplanetary environment
→ Result: Magnitude of interaction of the Didymos system with interplanetary magnetic fields,
detection of temporary megnetoshpere
→ Result: Determine the magnitude of solar wind ion disturbances/interaction with the binary
asteroid (Didymos system)
8. Determine mass of Didymos I and II from APEX orbit perturbations
→ Result: Mass of Didymos I and II
9. Determine strength of the near-surface material from APEX landing
→ Result: Surface material strength
AIDA target –binary asteroid Didymos
• Primary (Didymain) diameter 780 m, 2.1 g/cm3
• Secondary (Didymoon) diameter 160 m
• S-type composition
• Distance between centers 1.2 km
• Orbital period 12 h
• Apollo type NEA (Near-Earth Asteroid)
Radar shape, Benner and Naidu Shape model, Schwartz
• 6U configuration
• On-board data processing
• 15 kg, 15 W
APEX CubeSat
• New interplanetary AOCS
(Attitude and Orbit Control
System)
for semi-autonomous operations
and navigation includes:
→ 3-axis IMU (Inertial
Measurement Unit)
→ Propulsion
→ Reaction wheels
→ LIDAR
→ Navigation camera
AIDA scenario
The joint ESA-NASA AIDA project to binary asteroid Didymos
consists of Hera (ESA) and DART (Double Asteroid
Redirection Test, NASA). DART is targeted to impact Didymos
secondary component (Didymoon) and serve as a kinetic
impactor to demonstrate deflection of potentially hazardous
asteroids. Hera will serve as an observational spacecraft to
evaluate the effects of the impact and resulting changes in the
Didymos dynamic parameters.
The Hera mission will also carry APEX 6U CubeSat. This
arrangement opens up a possibility for secondary scientific
experiments. ASPECT aims to study the composition and
internal structure of the Didymos binary asteroid, effects of
space weathering, and DART impact crater and ejecta
distribution, in order to gain understanding of the formation and
evolution of the Solar System.
Didymos
Composition
ASPECT – mineralogy
ACA – chemistry
MAG - FeNi
Surface
ASPECT – roughness, space
weathering, ejecta
ACA – Solar wind interaction
Interior
MAG – internal structure
APEX
ESA - NASA -
A ID
A
• DLR, Bremen
• Space Systems Czech (SSC)
• The Czech Academyof Sciences
• Swedish Instituteof Space Physics (IRF)
• V-kvadrat AB
• Royal Instituteof Technology (KTH)
• OHB Sweden
• LC ISR, Ukraine
• Reaktor Space Lab (RSL)
• Aalto University
• VTT Research Centre of Finland Ltd
• University of Helsinki
APEX
AIDA scenario ASPECT
4 independent measurement channels:
VIS (500–900 nm, 1024 x 1024 px)
NIR1 (900–1600 nm, 640 x 512 px)
NIR2 (1600–2500 nm, 640 x 512 px)
Fabry-Perot Interferometer, 45 nm spectral resolution
1 m/px at 4 km, 3 cm/px at 200 m
MAG
Proximity measurements ( 100
FoV 40° full width cone
ASPECT VIS-NIR hyperspectral imager
ACA sputtered ion analyzer
MAG dual sensor magnetometer