We propose a three-year cubesat mission, daili, to study dynamical changes in the earth's atmospheric composition in the approximate 140 to 290 KM altitude region. Daili implements a newly developed…

Ended Grant For Research Awarded Last action

Contract number
80NSSC18K0973
Awardee
Awarding agency
Obligated
$3,104,718

Award facts

Contract value 100% obligated
$3,104,718.02 Current and potential, with all options
Completion date 100% complete
Current and potential, with all options
NAICS code
Not on record
Set-aside
No set-aside
Competition
Full and Open Competition Basic Research
Pricing
Other
Place of performance
LOS ANGLS AFB, CA 90009, USA

Award details come from SAM.gov/FPDS.

Transactions

Action Obligated Date
Funding Only Action P00008 -$731
Other Administrative Action P00007 $0
Funding Only Action P00006 $252,442
Other Administrative Action P00005 $0
Other Administrative Action P00004 $0
Other Administrative Action P00003 $0
Funding Only Action P00002 $530,724
Funding Only Action P00001 $1,360,497
Original award $961,786

About this award

This is a $3,104,718.02 grant award from the National Aeronautics and Space Administration (NASA) to The Aerospace Corporation, a federally funded research and development center (FFRDC), to conduct a 3-year CubeSat mission called DAILI. The mission will study dynamical changes in the Earth's atmospheric composition in the 140 to 290 km altitude region, utilizing a new technique to measure absolute oxygen density. The data will be used to evaluate and improve atmospheric models. The grant supports NASA's strategic goal of advancing the understanding of fundamental physical processes of the space environment. There is no set-aside designation for this award.

Description

We propose a three-year cubesat mission, daili, to study dynamical changes in the earth's atmospheric composition in the approximate 140 to 290 KM altitude region. Daili implements a newly developed technique, recently published in GRL, to measure the absolute O2 density at mid and low latitudes. The technique utilizes the ratio of two bright dayglow emissions, a portion of the O2A (0,0) band at 765 NM and the OI redline at 630 NM. This will allow the first comprehensive measurement of O2 density in the 140 to 200 KM altitude regime (the thermosphere GAP region) where atmospheric neutral density measurements are scarce. The redline is also sensitive to ionospheric density at altitudes above 200 KM, so this technique will also provide daytime/nighttime ionospheric data for comparison to models. Variations of the altitude profiles of O2 and the redline can be used to study tidal and planetary wave variability throughout the measurement regime as well as transport of neutral O2 from high to low latitudes due to geomagnetic activity. The data will be compared to state-of-the art models to help in their evaluation. Daili will address the following science objectives. (1) 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. (2) measure the altitude variability of tides and planetary waves from 140 to 180 KM where measurements by other means are scarce. (3) determine the latitudinal and altitudinal extent of the transport of neutral O2 during geomagnetically active periods. (4) determine variations in the f-region electron density profile in response to tides and planetary waves above 200 KM. The 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 x 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. The daili data rate will be about 5 mbytes/day. 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. The design life of daili is at least one year. The received data will be stored and processed at aerospace and then compared to state-of-the art models including auric, timed GCM and glow to meet the objectives. The daili experiment directly addresses NASA s strategic goal 2.2, to study the sun and its interactions with the earth and the solar system, in particular, the goal of advancing understanding of fundamental physical processes of the space environment. The composition and ionospheric data provided by daili will further our understanding of such processes in the lower thermosphere, where measurements are scarce. 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 of both the neutral density and the ionosphere.

Quick answers

Who was awarded contract 80NSSC18K0973?

80NSSC18K0973 was awarded to The Aerospace Corporation by Shared Services Center (National Aeronautics and Space Administration) on May 23, 2018.

How much is contract 80NSSC18K0973 worth?

The government has obligated $3,104,718 on 80NSSC18K0973.

Was contract 80NSSC18K0973 competed?

The extent of competition for 80NSSC18K0973 was full and open competition.

On GovTribe

See this award's full record

  • Every transaction and funding action
  • The awardee's other awards and teaming partners
  • Similar awards and recompete opportunities
  • Ask GovTribe AI about this award