HaWK High Watts per Kilogram Solar Arrays
Rigid-panel deployable solar arrays delivering 36 W to 330 W, flight-proven on defense, exploration, and commercial missions including NASA's MarCO interplanetary CubeSats.
Typed specifications11 values
Discloses 2 of 12 fields engineers filter by in this category (category median 3).
- Output power (BOL)
- 36 W product page 36 W min · HaWK range: from 36 W to 330 W | 330 W max · HaWK range: from 36 W to 330 W; 330 W per wing
- Deployable
- yes deployment success rate, stows on a CubeSat · datasheet p.1
- Power consumption
- 36 W product page
- Flight heritage
- Flight heritage configurations; HaWKs have flown on platforms from MicroSats to SmallSats, in VLEO, LEO, GEO, CisLunar orbit, heliocentric and a Mars flyby; 100% deployment success rate datasheet p.2
- Satellite class
- CubeSat CubeSat Solar Arrays; stows on a CubeSat · datasheet p.2 microsat 10-100 kg have flown on a variety of platforms from MicroSats to SmallSats | microsat 10-100 kg | smallsat 100-500 kg have flown on a variety of platforms from MicroSats to SmallSats | smallsat 100-500 kg
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier3 lines, in the manufacturer's own wording
- Power output range
- 36 W to 330 W
- Panel type
- Rigid deployable panel
- Flight heritage
- NASA MarCO interplanetary mission, defense and commercial missions
About
MMA Space’s HaWK (High Watts per Kilogram) solar arrays are rigid-panel deployable power systems spanning an output range of 36 W to 330 W. The line has supported defense, exploration, and commercial missions, including NASA’s MarCO interplanetary mission — the first CubeSats to operate beyond Earth orbit. HaWK arrays are designed, fabricated, assembled, and tested in-house at MMA’s Colorado headquarters, providing high specific power for mass-constrained smallsat and CubeSat platforms requiring dependable, flight-proven power generation.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.