Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.


DAILI [The Aerospace Corporation]

The DAILI (Daily Atmospheric Ionospheric Limb Imager) mission is a scientific investigation mission that studies dynamic changes in Earth's neutral/ionosphere density in the ~140 km - 290 km altitude region. The satellite built by The Aerospace Corporation is a 1×6U CubeSat.

The wide spatial and temporal distribution of the data provided by DAILI over the course of its mission will improve the accuracy of operational models for both the neutral density and the ionosphere, and will help further the study of wave propagation and transport processes in the lower thermosphere.

The DAILI mission will study the atmosphere at an altitude range of about 140 to 290 kilometers. In this region, measurements are scarce, and density and composition are highly variable. This variability affects the plasma and atmospheric structure at higher orbital altitudes. DAILI will provide data for atmospheric models, important for applications such as calculating the precise orbits of satellites and understanding the propagation of radio signals.

This technique was validated by previous measurements made by Aerospace’s photometer portion of the Remote Atmosphere/Ionosphere Detection Sensor (RAIDS), which was deployed on the International Space Station. DAILI provides the same capability as RAIDS in a miniature form.

DAILI will address the following science objectives:

  • Determine the O2 density from 140 to 180 km at mid and low latitudes on a daily basis and compare with models such as MSIS and TIME-GCM.
  • Measure the altitude variability of tides and planetary waves from 140 to 180 km where measurements by other means are scarce.
  • Determine the latitudinal and altitudinal extent of the transport of neutral O2 during geomagnetically active periods.
  • Determine variations in the F-region electron density profile in response to tides and planetary waves above 200 km.

The DAILI mission will complement two NASA satellite missions, ICON and GOLD.

The linear six-unit (10x10x60 cm) (1×6U) DAILI payload consists of a two-channel photometer, occupying about 2 U, that images the Earth's limb over a 6 degree FOV onto different regions of a single CCD, each color channel occupying about 180 × 180 pixels. At a nominal limb distance of 2300 km the FOV is nominally from 140 to 290 km in altitude over a 150 km horizontal span. A sunshade, which occupies about 3U exterior to the optics, excludes scattered light from the Sun, the hard Earth and low altitude clouds. The Aerospace CubeSat bus takes up the remaining space. The bus satisfies all power, thermal and pointing requirements for camera operation, including a star sensor and attitude control system capable of payload pointing to better than 0.1 degree. This pointing system will allow higher or lower altitudes than the nominal range to be observed, if desired.

DAILI will be designed, built, and flown by Aerospace and is scheduled to begin its one-year flight mission in 2020. It is proposed that DAILI be launched from the ISS, using the NanoRacks CubeSat Deployer, giving a nominal 51-degree inclination orbit at 400 km altitude.

It was selected in 2019 by NASA's CubeSat Launch Initiative (CSLI) to be launched as part of the ELaNa program.

The satellite was launched onboard the Dragon CRS-24 cargo spacecraft to the ISS, where it will be deployed later.

Nation: USA
Type / Application: Science, ionosphere
Operator: The Aerospace Corporation
Contractors: The Aerospace Corporation
Configuration: CubeSat (1×6U)
Power: 2 deployable fixed solar arrays, batteries
Lifetime: 1 year
Mass: x kg
Orbit: 409 km × 421 km, 51.64°
Satellite COSPAR Date LS Launch Vehicle Remarks
DAILI 1998-067TF 21.12.2021 CCK LC-39A Falcon-9 v1.2 (Block 5) with Dragon CRS-24, STP-H7, STP-H8, PATCOOL, TARGIT, GASPACS, Light 1, GT 1, FEES 2


Cite this page: