MarCO - Utah State University

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MarCO CubeSats to Mars in 2016 Andrew Klesh [email protected]

Transcript of MarCO - Utah State University

Page 1: MarCO - Utah State University

MarCOCubeSats to Mars in 2016

Andrew [email protected]

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MarCO Fast Facts:• 2 x 6U (14 kg) spacecraft launching as auxiliary payloads on InSight’s Atlas V-401• 27 day launch window in March 2016• Separation approximately 95 min after launch• 6.5 month cruise (157 million km) to Mars• 5 Trajectory Correction Maneuvers to establish Mars-flyby heliocentric orbit• Flying by Mars September 28, 2016

Mission Objective:• Provide an 8kbps real-time relay for

InSight’s 2016 Entry, Descent and Landing at Mars

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March 2016

Mars

Earth

Sept 28, 2016Entry, Descent, and Landing

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Mars

Earth

March 2016

Sept 28, 2016Entry, Descent, and Landing

TCM 1

TCM 2

TCM 3

TCM 4

TCM 5

6.5 Month Cruise

157,077,764 km

MarCO

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High Gain Reflectarray (JPL)

X-Band Transponder (JPL)

Solar Arrays (MMA)

SSPA & LNA (JPL)

Cold Gas Thrusters (Vacco)

CDH & EPS (AstroDev)

Attitude Control (BCT)

MGA, LGA,Structure (JPL)

MarCO Overview:Volume: 2 x 6U (10x10x30cm)Mass: 14.0 kgPower Generation:

Earth: 35 WData Rates: 62-8,000 bpsDelta-V: >40 m/s

Software:FSW: protos (JPL)GSW: AMPCS (NASA/JPL)

I&T:In-house S/C I&T, testing, Tyvak NLAS/Launch Integration

Operations: Primary: DSN 34mEDL: Madrid 70m

Mission Objective:• Provide an 8kbps real-time

relay for InSight’s Entry, Descent and Landing at Mars

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MarCO Overview:Volume: 2 x 6U (10x10x30cm)Mass: 14.0 kgPower Generation:

Earth: 35 WData Rates: 62-8,000 bpsDelta-V: >40 m/s

Software:FSW: protos (JPL)GSW: AMPCS (NASA/JPL)

I&T:In-house S/C I&T, testing, Tyvak NLAS/Launch Integration

Operations: Primary: DSN 34mEDL: Madrid 70m

Mission Objective:• Provide an 8kbps real-time

relay for InSight’s Entry, Descent and Landing at Mars

UHF Antenna (JPL)

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Thermal Blanket

Mechanical Fit Check• Includes all external flight-like hardware• Pre-validate NLAS-II Canister fit

Thermal Radiator (JPL)

Tyvak NLAS-II Canister (with MarCO) Vacco Thruster Blue Canyon Technologies ADCS

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MarCO-A

MarCO-B

UHF RelayDSN 70mReception

Sept 28, 2016InSight Entry, Descent, and Landing

157,077,764 km

3,500 km

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CubeSats at MarsArriving 2016

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© California Institute of Technology. Government sponsorship acknowledged.