The Asteroid Impact & Deflection Assessment (AIDA) mission is a joint project of ESA and NASA. It is a technology demonstration of the kinetic impactor concept to deflect a small asteroid and to characterize its physical properties. It started in 2011 as a joint study between JHU/APL, NASA, the Côte d’Azur Observatory (OCA, Nice, France) and DLR. The mission went into phase A/B1 at ESA in early 2015 for 15 months and will enter into Phase A at NASA in spring 2015 (see News below). You can watch the Video explaining the concept on the ESA website (click here).
AIDA is composed of the projectile called DART (Double Asteroid Redirection Test) and an observer satellite called AIM (Asteroid Impact Mission), each under study by NASA and ESA, respectively.The combination of both spacecrafts is referred to as AIDA. As in the separate DART and AIM studies, the target of this mission is the binary asteroid system (65803) Didymos. For a successful joint mission, one spacecraft, DART would impact the secondary of the Didymos binary system in October 2022 while AIM would first characterize the target asteroid (surface and internal properties), observe the impact event and measure any change in the relative orbit.
Another Video made by the APL/JHU laboratory (USA), in which a few involved scientists and engineers explain the motivation, is posted on YouTube (click here)
NEWS:/MEETINGS (upcoming in yellow)
- 2nd AIDA International Workshop in Nice (France), June 1-3, 2016 (click here for more information).
- European Geoscience Union (EGU) General Assembly 2016: PS1.5 Science and Technology for the Asteroid Impact & Deflection Assessment (AIDA) mission (Vienna, Austria), April 17-22, 2016 (click here for information)
- Asteroid Impact Mission (AIM) Science Meeting in ESAC (Madrid, Spain), March 1-2, 2016 (click here for information)
- Public AIDA splinter meeting at the European Planetary Science Conference (EPSC) 2015 on Sept. 29th, at 17:45 (room Mars); click here for info from ESA web site.
- The study of AIM by ESA is now in Phase A/B1 since early March 2015 for 15 months (click here for more info).
- Two industrial studies as well as payload studies are performed (click here for more info).
- A call for cubesat experiments (closed) has also been released (click here for more info).
- The AIM investigation team led by P. Michel (CNRS/Côte d’Azur Observatory, France), composed of scientists with the different required expertises, define the science objectives, requirements, and environment.
- The DART investigation team is led by A. Cheng (APL/JHU). DART is in pre-Phase A and is planed to go into Phase A in early fall 2015.
The Asteroid Impact & Deflection Assessment (AIDA) mission will be the first space experiment to investigate a binary near-Earth asteroid (NEA) and to demonstrate asteroid impact hazard mitigation by using a kinetic impactor. AIDA is a joint ESA-NASA cooperative project, which includes the ESA Asteroid Impact Mission (AIM) rendezvous spacecraft and the NASA Double Asteroid Redirection Test (DART) mission. The primary goals of AIDA are:
- to investigate the binary NEA (65803) Didymos;
- to test our ability to impact its moon by an hypervelocity projectile in 2022 and
- to measure and characterize the impact deflection both from space with AIM and from ground based observatories.
The two concepts (DART projectile and AIM orbiter) are developed as two self standing missions. Joining the two missions will allow performing an impact (DART) in order to deflect the smaller component of the asteroid binary system in October 2022 and observe the impact crater and derive collision and impact properties (AIM).
AIM is a rendezvous mission that focuses on the monitoring aspects i.e., the capability to determine in-situ the key properties of Didymos’ satellite used as the target of the deflection test. AIM will also give access to the detailed conditions of the DART impact and its outcome, allowing for the first time to get a complete picture of such an event, a better interpretation of the deflection measurement and a possibility to compare with numerical modeling predictions. Baseline payloads for AIM include the following remote sensing and in-situ instruments: a Visual Imaging System, a lander (based on DLR MASCOT heritage), a thermal infrared imager, a high frequency (decimeter-wave) radar, and a low frequency (60 MHz) radar, to measure Didymos surface and sub-surface physical properties and to study internal structures. AIM also includes an optical communication demonstration that can be used as a laser altimeter and CubeSat payloads.
AIM is not meant to be a purely scientific mission but rather a technology demonstration. However, AIM will improve drastically our scientific knowledge on small asteroids, in very relevant areas of Solar System science, such as asteroid geophysics, granular mechanics, impact processes, and thermal effects/properties.
The primary goals of DART are (i) to demonstrate a hypervelocity spacecraft impact on a small near-Earth asteroid (NEA) and (ii) to measure and understand the deflection caused by the impact.
The DART mission includes ground-based optical and radar-observing campaigns of Didymos both before and after the kinetic impact experiment, as well as modeling and simulation programs. DART has the further objective to learn how to mitigate an asteroid threat by kinetic impact and to develop and validate models for momentum transfer in asteroid impacts. AIM will further make detailed measurements of the DART impact and its outcome.
AIM + DART
The DART and AIM missions, comprising AIDA, will return fundamental new information on a binary system, on its mechanical response, on the impact cratering process, and consequently on the collisional evolution of asteroids with implications for planetary defense, human spaceflight, and Solar System science. AIDA mission studies involve various scientific activities regarding binary dynamics and impact modeling, asteroid geophysics, observations. AIDA will be the first fully documented impact experiment at real asteroid scale, allowing numerical codes to be tested and used for similar and other scientific applications at those scales.