EuCROPIS

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Eu:CROPIS
Life sciences research
OperatorGerman Aerospace Center[1]
COSPAR ID2018-099BB Edit this at Wikidata
SATCAT no.43807Edit this on Wikidata
Mission durationPlanned: 1 year[1]
Final: 1 year and 28 days
Spacecraft properties
BusDLR Compact Satellite bus[2][3]
ManufacturerDLR
Launch mass250 kg (550 lb)[1][3]
Dimensions1.0 m diameter x 1.13 m length[3]
with panels deployed: 2.88 m wide[3]
Power520 W, 4 solar arrays, Li-ion batteries[1][3]
Start of mission
Launch date3 December 2018
Vandenberg Air Force Base
ContractorSpaceX[6]
End of mission
DisposalDecommissioned
Deactivated31 December 2019
Orbital parameters
Reference systemGeocentric
RegimeLow Earth (SSO)
Perigee altitude575 km (357 mi)[3]
Inclination98°[2][3]
Period10 h
EpochPlanned[5]
Transponders
BandS band[3]
 

Eu:CROPIS (Euglena and Combined Regenerative Organic-Food Production in Space) was a life science satellite developed by the

sustainable food
source using human urine for moisture and as the source of fixed nitrogen.

Overview

This orbital mission was intended to simulate and teste two

life support system functioning in low gravity.[7]

In more detail, porous lava stones were fitted in trickle filters and dried soil containing normal soil microbial colonies. Microbes would then use nitrite (NO
2
) to convert the harmful ammonia (NH
3
) into nitrate (NO
3
), which is then added to six tomato seeds as liquid fertiliser.[6] In addition, the system incorporated a colony of the single-cell microorganism Euglena gracilis, a photosynthetic algae able to produce oxygen and biomass while protecting the entire system against high ammonia concentrations.[6][7] This oxygen is necessary for the conversion of urine to nitrate until the photosynthetic oxygen production by the tomatoes is sufficient.[7]

The spacecraft was designed replicate lunar gravity on one greenhouse for a period of six months before simulating Martian gravity on the second greenhouse for the next six months.[6] The level of gravity on the Moon (0.16 g) and Mars (0.38 g) was simulated by rotating the spacecraft's cylindrical body around its longitudinal axis.[1] The various payload experiments were placed in different areas within the cylinder.[3] Tomato seed germination and plant growth were monitored with 16 cameras,[6] while the RAMIS (RAdiation Measurement In Space) radiometers monitored the radiation inside and outside the spacecraft.[6][7]

The greenhouse was made of clear polycarbonate, with an approximate volume of 12 L (730 in3).[7] The closed system featured moisture, pH, oxygen, pressure and temperature sensors, and was capable of controlling these parameters. Four small fans created airflow through a cooling device to maintain a stable "atmospheric" temperature. On top of the greenhouse, three lamps provided light in the correct spectrum for photosynthesis.[7] Scanners and fluorometers measured cell density and photosynthetic yield. The fluids were to be monitored with seven electrodes to measure ammonium, nitrite, nitrate, pH, chloride, sodium, and potassium.[7]

To monitor the health of Euglena gracilis, the system also analysed the microbes'

genes— were being commanded into action.[7]

Objectives

The aim was to develop a stable, and

life support system while being exposed to gravity levels similar to those on the lunar surface as well as the surface of Mars. Both phases of experimentation would last for six months.[7] With water being the only component that has been recycled so far and all other components being extracted and disposed, processing of urine is an issue in human space flight. Eu:CROPIS was intended to examine the possibility of using previously disposed waste to grow fruits and vegetables after proper conversion. Two life support systems (a nitrifying trickle filter system and the single-celled algae Euglena gracilis) within the satellite were to be used for producing biomass out of artificial urine in a closed system. Furthermore, the algae Euglena gracilis would protect the biosystem against high levels of ammonia present in urine.[3]

Supporting science payloads

Satellite characteristics

Both the satellite and the experiment are called Eu:CROPIS. The satellite features four gyroscopes, two magnetometers, three magnetic torque rods and a Sun sensor in combination with a single-frequency Phoenix GPS receiver for attitude control.[3][10] The power for the satellite is provided by an Electrical Power Subsystem, which includes a lithium-ion battery and four deployable fixed solar arrays delivering an average of 520 W of power.[1]

Results

The Eu:CROPIS mission ended on 31 December 2019. The three supporting payloads generated large amounts of data, but the eponymous Eu:CROPIS experiment failed to activate due to a software problem. The satellite is expected to slowly de-orbit over the next two decades before reentering Earth's atmosphere.[11]

See also

References

  1. ^ a b c d e f g "Eu:CROPIS". space.skyrocket.de. Retrieved 2018-09-26.
  2. ^ a b Institute of Space Systems, Status Report 2007-2016. (PDF) DLR.
  3. ^ a b c d e f g h i j k l m "Eu CROPIS - eoPortal Directory - Satellite Missions". directory.eoportal.org. Retrieved 2018-09-26.
  4. ^ "SpaceX Twitter". twitter.com. 2018-12-02.
  5. ^ a b "UNITED STATES COMMERCIAL ELV LAUNCH MANIFEST". sworld.com.au. 2018-09-26.
  6. ^ a b c d e f g DLR. "Eu:CROPIS – Greenhouses for the Moon and Mars". DLR Portal. Retrieved 2018-09-26.
  7. ^
    ISSN 0938-0108
    .
  8. ^ Kovo, Yael (2015-11-09). "PowerCell". NASA. Retrieved 2018-09-26.
  9. ^ "Food Production in Space - Operating a Greenhouse in Low Earth Orbit (PDF)". nasaspaceflight.com. 2016-05-20. Retrieved 2018-09-26.
  10. ^ Attitude Control System of the Eu:CROPIS Mission. (PDF) Ansgar Heidecker, Takahiro Kato, Olaf Maibaum, Matthew Hölzel. DLR Institute of Space Systems.
  11. ^ "Farewell to the Eu:CROPIS mission". DLR. 13 January 2020. Retrieved 4 December 2020.