Some details about this mission provided by the wonderful Seager Yu. Below is a reproduction of the information he has provided, summarized and adapted for the format of a forum post, and hopefully given a bit more permanency than what one finds on Twitter.
The architecture of Chang'e 7 appears pretty similar to the Chang'e 5/6 missions. The target landing site is 88.8° S 123.4° E. The instrument descriptions are taken from
this LPSC presentation. It also outlines the objectives of the mission:
QUOTE
The Chang'e 7 mission, scheduled for 2024, is the first mission in the follow-up missions (i.e., CE-6, 7, 8) of CLEP. The scientific objectives of the mission include:
(i) Obtaining information of lunar inner ring [sic] structure, mineral and element components, the characteristic of the electric and magnetic fields, heat flow and gravitational field,
(ii) Obtaining the distribution and source of lunar water and volatiles, directly confirming the presence and source of water ice on the Moon;
(iii) Imaging the energetic neutral atoms with high space-time and energy resolution of the Earth's magnetotails and understanding the dynamics of the Earth's magnetotails,
(iv) Researching the space environment such as the lunar surface magnetic field, lunar dust and particle radiation, revealing the mechanism of solar wind causing the magnetic anomalies in the vortex region of the lunar surface.
Chang'e 7 has a relay satellite, a lander, a rover and a "mini-flying probe," which all together will have 23 payloads, with a total mass of 8200 kg. The Chang'e 7 relay satellite will facilitate communication with the south polar region of the Moon.
Click to view attachmentThis is the Chang'e 7 orbiter. It has the following instruments.
- High Resolution Stereo Mapping Camera (high-precision topography of the lunar surface)
- Miniature Synthetic Aperture Radar (high-precision topography of the lunar surface and permanently shadowered areas)
- Wide-Band Infrared Spectrom Mineral Imaging Analyzer (high-precision mineral composition and surface thermal environment)
- Lunar Neutron Gamma Spectrometer (high-precision characteristic gamma ray and neutron flow data for lunar surface)
- Lunar Orbit Magnetometer (combined with rover to study lunar micromagnetosphere)
Click to view attachmentThis is the Chang'e 7 lander. It carries the following instruments:
- Landing camera (landing area and topography data)
- Topography Camera (landing area topography data)
- In-Situ Measuring System of Volatiles and Isotopes on Lunar Surface (in-situ exploration of volatiles in the landing area)
- Lunar Soil Section Thermal Current Measuring (measuring the lunar soil heat flow)
- Lunar Surface Thermometer (Measure the temperature of lunar surface)
- Extreme Ultraviolet Camera (obtain imaging data of the earth plasma layer)
- Lunar seismograph (obtain lunar seismic data on the south pole)
On top of the lander, we see FYQ-1. Mounted on the side we see Yutu 3.
Click to view attachmentThis is Yutu 3, carried with Chang'e 7. It carries four scientific payloads:
- Panoramic Camera (obtain topographic data on the rover area)
- Rover magnetometer (obtain the magnetic field and its gradient change in the rover area)
- Lunar Penetrating Radar (obtain data of shallow structure of lunar soil in the rover area)
- Lunar Raman Spectrometer (obtain data on mineral composition on the rover area).
Click to view attachmentThis is the FQY-1 (飞跃器一号, which translates to something like "hopper-1"). According to Seger Yu, in addition to being a walker, it has a propulsive system allowing it to make three "hops."
The first hop appears to be a test and will fly in the vicinity of the Chang'e 7 lander and Yutu 3 rover, taking images of the two. The second hop will be into a permanently shadowed crater. The third hop will get itself out of the permanently shadowed area. From this point onward it can walk around and function effectively as a second rover.
It's instrument payload appears to be restricted to a single hydrogen isotope and water molecule detector.