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PAS 610S (24") Separation System Low Shock Satellite Separation System for your mission The load capability of the RUAG PAS 610S Separation System is fully compatible with the Moog CSA ESPA and environments from the ESPA Rideshare User's Guide (ESPA RUAG). The Separation System includes a low shock clamp band separation system, inter- face rings, umbilical connection and a separation spring set. With our CBOD-LT™ Separation System Release Mechanism we can provide the unique combination of high load capability and a low shock release. Building on heritage and reliability The PAS 610S Separation System is based on the already flight proven systems at RUAG. Developed for over 30 years, the RUAG Space product family to date includes a broad range of Separation Systems, spanning diameters from 381 mm to 2624 mm (15" to 103"). Our Separation Systems have an outstanding flight record. To date more than 550 in-orbit separations have been carried out with a success rate of 100%! Our customer base includes launch service providers, satellite builders, government entities and national space agencies. We work closely with the custom- ers during the spacecraft design phase to establish a fully com- patible design. 0 0,5 1 1,5 2 0 200 400 600 800 1000 CoG [m] (1m = 39.4 inch) S/C Mass [kg] (1 kg = 2.2 lbm) S/C Mass - CoG Envelope a (lateral) = 8,5 g

RUAG | RUAG - PAS 610S Separation System...the ESPA Rideshare User's Guide (ESPA RUAG). The Separation System includes a low shock clamp band separation system, inter-face rings, umbilical

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Page 1: RUAG | RUAG - PAS 610S Separation System...the ESPA Rideshare User's Guide (ESPA RUAG). The Separation System includes a low shock clamp band separation system, inter-face rings, umbilical

PAS 610S (24") Separation System

Low Shock Satellite Separation System for your missionThe load capability of the RUAG PAS 610S Separation System is fully compatible with the Moog CSA ESPA and environments from the ESPA Rideshare User's Guide (ESPA RUAG). The Separation System includes a low shock clamp band separation system, inter-face rings, umbilical connection and a separation spring set. With our CBOD-LT™ Separation System Release Mechanism we can provide the unique combination of high load capability and a low shock release.

Building on heritage and reliabilityThe PAS 610S Separation System is based on the already flight proven systems at RUAG. Developed for over 30 years, the RUAG Space product family to date includes a broad range of Separation Systems, spanning diameters from 381 mm to 2624 mm (15" to 103").

Our Separation Systems have an outstanding flight record. To date more than 550 in-orbit separations have been carried out with a success rate of 100%! Our customer base includes launch service providers, satellite builders, government entities and national space agencies. We work closely with the custom-ers during the spacecraft design phase to establish a fully com-patible design.

0

0,5

1

1,5

2

0 200 400 600 800 1000

CoG

[m] (

1m =

39.

4 in

ch)

S/C Mass [kg] (1 kg = 2.2 lbm)

S/C Mass - CoG Envelopea (lateral) = 8,5 g

Page 2: RUAG | RUAG - PAS 610S Separation System...the ESPA Rideshare User's Guide (ESPA RUAG). The Separation System includes a low shock clamp band separation system, inter-face rings, umbilical

Illustrative Drawing and Nominal Release Envelopes

RUAG Space | ASJ-vägen 9 | Box 1134 | SE-581 11 Linköping | SwedenPhone +46 13 482 84 00 | Fax +46 13 482 84 98 | [email protected] | www.ruag.com/space

Main characteristics of PAS 610S

Unit Value

Bolt pretension (nominal) kN 15

Mass Total 1) kg 5.8

Separated mass kg 1.0

Dimensions Height 2) mm 73

I/F Passive ring 36 x 1/4 inch bolt holes on a diameter of 609.6 mm (24 inch, ESPA Grande)

Active ring 36 x 1/4 inch bolt holes on a diameter of 609.6 mm (24 inch, ESPA Grande)

Initiator type Pacifi c Scientifi c 103377-449Hi-Shear PC23-250ASI PD22240024-009USI 1F01084-1

Separation springs No. of springs pcs 4 to 10

Spring energy 3) Joule 4.7

Release type CBOD-LT

Shock output Low shock < 100 g's @ 1 kHz

1) Mass of the standard system including passive ring. Can be optimized to meet specifi c needs.2) Height only includes active and passive ring.3) Energy per spring.

R - R

S - S