Quadro Arrow

Typed specifications66 values

Discloses 8 of 14 fields engineers filter by in this category (category median 1).

Mass

8.4 kg

Arrow 150 combined stowed mass · datasheet p.4 6.82 kg Arrow 150 L-Adapter  |  1.58 kg Arrow 150 S-Adapter (all four points)  |  8.4 kg Combined Mass  |  8.4 kg Combined Stowed Mass  +8

Preload / holding force

0.07 kN

Holding force · datasheet p.18 75 kN max · Maximum Axial  |  75 kN max · Maximum Axial Force  |  20 kN max · Maximum Lateral (Shear)  |  20 kN max · Maximum Shear Force

Release time

500 ms

Nominal Pulse Duration · datasheet p.18 100 ms Average Separation Time

Supply voltage

28 V

Nominal Voltage · datasheet p.18 24 V min  |  36 V max

Operating temperature

-34 °C

Lower Operating Limit · datasheet p.4 71 °C Upper Operating Limit  |  -34–71 °C operating limits

Export status

ITAR-free

datasheet p.6 not controlled not subject to export restrictions of any kind

Separation type

point separation bolts or nuts

datasheet p.6 other four-point hold-down and release mechanism (HDRM) with perman…  |  other HDRM

Number of bolts or points

4

four-point system, four HDRM points · datasheet p.6 16 number of fasteners, Arrow 150

Max spacecraft mass

300 kg

datasheet p.6 150 kg min · suitable for microsatellites between 150kg and 800kg  |  800 kg max · suitable for microsatellites between 150kg and 800kg  |  300 kg max · suitable for satellites weighing up to 300 kg flying on Falco…

Tip-off rate

0.6 °/s

average rotation rate across all three axes, satellites deplo… · datasheet p.16 2.22 °/s Max tip-off rate  |  2.22 °/s max · max tip-off rate in Table 5 of customer-reported values  |  2 °/s max · no axis rotation higher than 2 deg/s recorded from satellites…

Release command type

voltage pulse

Nominal Separation Signal · datasheet p.4 voltage pulse deploy command to permanent electromagnets, 24VDC for 0.5s

Release actuator voltage

24 V

nominal separation signal 24VDC for 0.5s · datasheet p.4 24–36 V permanent electromagnet voltage range  |  28 V nom. · permanent electromagnet nominal voltage

Command pulse duration

500 ms

Nominal Pulse Duration · datasheet p.18 500 ms nominal separation signal 24VDC for 0.5s  |  500 ms nom. · nominal pulse duration

Connector

two male DSub-9 connectors (Harting 09674095615) on the locking mechanism

datasheet p.17

Survival temperature

-55 °C

Lower Survival Limit · datasheet p.4 130 °C Upper Survival Limit  |  -55–130 °C survival limits

Flight heritage

Critical subsystems like lock mechanism and pusher arms have flight heritage across dozens of missions.

datasheet p.6

Satellite class

microsat 10-100 kg

up to 300 kg · datasheet p.6

Separation switches, count

2

internal telemetry switches: Clamp Ring TM1 and Pusher Arm TM… · datasheet p.17

Release command (as printed)

24VDC for 0.5s (nominal separation signal)

datasheet p.4

Release current

0.28 A

Nominal Separation Current · datasheet p.18 0.5 A Maximum Current  |  0.16 A Minimum All-fire Current  |  0.16 A min · minimum all-fire current  |  0.5 A max · maximum current  +2

Max bending moment

1 150 N·m

per HDRM, Arrow 150 · datasheet p.4

Launch vehicles

Falcon 9

satellites flying on Falcon 9 Rideshare plates · datasheet p.6

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. Report a wrong value