Citation:
Chiara Palla, Jenny Kingston, and Stephen Hobbs. Development of commercial drag-augmentation systems for small satellites. 7th European conference on Space Debris, 18 - 21 April 2017, ESA/ESOC, Darmstadt, Germany.
Abstract:
In the framework of the ESA CleanSat programme
Cranfield University is developing a family of drag
augmentation system (DAS) modules to enable small
satellites in Low Earth Orbit (LEO) to comply with space
debris mitigation requirements.
There are currently two mature Cranfield DAS designs
based on deployable Kapton sails using stored energy
for deployment. One concept is Icarus and it is currently
on-board the UK’s TechDemoSat-1 (launched 8 July
2014) and Carbonite-1 spacecraft (launched 10 July
2015). The second concept is the de-orbit mechanism
(DOM) module, which is due to fly as technological
demonstrator on the upcoming ESA ESEO mission.
The key drivers used during the design process were: low
cost, low mass, easy testability, safety, reliability, and
avoidance of additional debris production. These drivers
matched with top-level requirements, from a potential
customers perspective (e.g.: satellite integrators), which
were defined during the CleanSat study. Other relevant
requirements for the DAS included demisability, performance
(in terms of orbital decay), area-to-mass ratio,
functionality, lifetime, and environment compatibility.
This paper discusses the compliance of the Cranfield
DAS designs with the identified requirements, and
illustrates the scalability via application to several case
study missions (500 kg and 200 kg LEO satellites).
The two most challenging aspects to assess were compliance
with the lifetime required for storage on ground
and pre-deployment on orbit, and the effect of the orbital
environment (radiation, ATOX, debris) on the sail.
The study has provided useful input to explore new
concepts based on the heritage designs; these concepts
are evolutions of the DOM unit and hybrid designs. The
hybrid design combines aspects of the Icarus and the
DOM concepts to reduce the limitations of the respective
individual devices and improve scalability, adaptability
and manufacturability.
In addition, this work is helping to achieve commercial
readiness for the technology. This will enable development
of a commercial DAS offering that will be an
attractive solution for small satellite integrators, allowing
them to meet debris mitigation requirements.