Redwire HiPASS – High-Power Rigid Array Solution for SmallSats
Redwire Corporation
SADA-compatible rigid solar array wing built for ESPA-class electric propulsion smallsat missions, using metallic tape-spring hinges.
Key figurescomparable across the catalogue
- Mass
- 17 kg
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Deployed wing dimensions
- 54 x 144 x 8 in (137 x 365 x 20 cm)
- Stowed wing dimensions
- 30 x 54 x 7.5 in (76 x 137 x 19 cm)
- Mass (1 kW point design)
- 17 kg
- Electrical arrangement (1 kW point design)
- 19s20p per wing, Spectrolab XTE 76.88 cm^2 cells
- Hinge type
- Metallic tape-spring hinges
- Drive compatibility
- SADA-compatible
- Panel material
- Low-cost graphite face-sheet panels
- Flight status
- 10 flight wings planned for delivery, multiple US Gov't missions
About
HiPASS (High-Power Rigid Array Solution for SmallSats) is Redwire’s tailored rigid solar array system engineered to support ESPA-class electric propulsion missions. The design uses metallic tape-spring hinges to create a robust wing that tolerates system-level tolerance stack-up, and is compatible with Solar Array Drive Assemblies (SADA). Low-cost graphite face-sheet panels are used to minimize manufacturing risk and cost.
A standard 1-kW point-design electrical arrangement uses a 19-series/20-parallel per-wing layout with Spectrolab XTE 76.88 cm-squared solar cells. HiPASS is a mature technology, with 10 flight wings for multiple U.S. Government missions planned for delivery.
Deployed, a HiPASS wing measures 54 x 144 x 8 inches (137 x 365 x 20 cm); stowed, it packages down to 30 x 54 x 7.5 inches (76 x 137 x 19 cm) at 17 kg mass for the 1-kW point design. Typical applications include solar array constellations, SADA-based spacecraft, smallsats, and ESPA-class electric propulsion missions.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.