Astralis Prototype 1

1. Mission Objective. Why do you need a propulsion system? Select all that apply.
Orbital Station Keeping (up to 3 years)
Long Orbital Station keeping (3+ years)
Travel to a designated orbit from GTO
Interplanetary or Lunar Travel
Pointing / Attitude Control
Collision Avoidance
Active Deorbiting at end of mission
Other
2. Size. How big will your satellite be (incl. The propulsion system)?
Up to 3U / 5 kg
6U / 10 kg
12U / 20 kg
16U / 25 kg
3. Launch Date. When will your mission launch?
2022
2023
2024 or later
4. Manoeuvres. What type of manoeuvres does your mission require?
High-Thrust / Impulsive
Precision / Low-thrust for a long time
Both
5. Delta-V Capability. What changes in velocity does the thruster(s) need to produce in order to carry out the manoeuvres required for your mission?
Less than 250 m/s
500 m/s
1 km/s
2 km/s
Over 3 km/s
6. Power. What power supply can your CubeSat use to operate the thruster?
20W
50W
100W
150W
200W
250W
7. Flight Heritage. You are more likely to consider a product that
Has been fully tested in space
Is new and highly innovative
No preference
8. Supplier Location. Do you have any preference regarding the location of the supplier?
Not really
USA
UK
EU
Other
9. Trade-offs. Select up to 5 system characteristics that are most important for your mission.
High specific Impulse
High Total Impulse
High Nominal Thrust
High Delta-V Capability
Long Operational Lifetime
Short Orbital Transfer Duration
Small Volume and Weight
Less Power Requirements
Excellent Supplier Reputation
Great Reliability and Heritage
High Radiation Tolerance
Fast Delivery Time
Affordable Price
Great Overall Performance
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