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ELSA-d

Jump to: Mission Objectives, Mission Instrumentation, Mission Parameters, Additional Information

Mission Images:

ELSA-d satellite
Image credit: Astroscale
Mission Objectives:

Scientific/engineering mission goal: The End-of-Life Service by Astroscale Demonstration (ELSA-d) mission's goal is to demonstrate end-of-life support and removal of semi-cooperative targets. Semi-cooperative means the target is equipped with a docking plate which allows for a less complex chaser. The idea is to have this docking plate mounted on future spacecraft, including large constellations. This would allow for reliable removal from orbit, even if the spacecraft does not reach it's designed end-of-life.

In order to find the target reliably, precise knowledge of its orbit is required. TLEs are not accurate enough. Astroscale thus promotes equipping future spacecraft with retro-reflectors especially for customers of their end-of-life support.

Role of SLR for the mission: The Satellite Laser Ranging will be used to perform Precise Orbit Determination of both Chaser and Target spacecrafts. This will allow the validation of relative ranging measurements that constitute the core of rendezvous & docking capabilities. It will also be vital for demonstrating the capability to find a semi-cooperative target. In the target search demo phase, SLR data will be used to get the chaser close enough for its proximity sensors to work.

The support of the ILRS network to precise orbit determination would be very welcome.

Mission Parameters:
Satellite Target Chaser
Sponsor: Astroscale Astroscale
Expected Life: 6 months 6 months
Primary Applications: Demonstrate end-of-life support and removal of semi-cooperative targets Demonstrate end-of-life support and removal of semi-cooperative targets
COSPAR ID:    
SIC Code: 4203 4204
NORAD SSC Code:    
Launch Date: April 2020 April 2020
RRA Size:    
RRA Shape:    
Reflectors: Hemispherical/Pyramid Hemispherical/Pyramid
Size of Reflector: 12.7 mm diameter, 10.10 mm height 12.7 mm diameter, 10.10 mm height
Orbit: eccentric eccentric
Orbital period: 95 minutes 95 minutes
Inclination: 97.6 degrees 97.6 degrees
Altitude: 500 - 600 km 500 - 600 km
Eccentricity: 0.001 .001

 

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