Deployers & Separation Systems — Space Hardware Marketplace — Page 2

CubeSat Deployers

Mercury-12T Tab-Based 12U CubeSat Dispenser

Maverick Space Systems

Price on request

Form factor 12 U

12U tab-based CubeSat dispenser delivering over 50% reduction in gRMS environment transmission, available now with flight-proven heritage.

CubeSat Deployers

Mercury-6T Tab-Based 6U CubeSat Dispenser

Maverick Space Systems

Price on request

Form factor 6 U

6U tab-based CubeSat dispenser delivering over 50% reduction in gRMS environment transmission, available now with flight-proven heritage.

Separation Systems

Maverick 4-Point Lightweight Separation System (M4P-L)

Maverick Space Systems

Price on request

Type4-point separation system
Payload classESPA class, up to 400 kg
Spring ratesTunable, to minimize tipoff

4-point separation system for ESPA class payloads up to 400 kg, with tunable spring rates, low shock and…

Deployers & Separation Systems

Separation Nut PSM 1/2B

Beyond Gravity (ex-RUAG Space)

Price on request

Target spacecraft classConstellation class satellites, typically 500-1000 kg
QualificationAIAA S-113-2005 (former DOD-E-83578A)
InitiatorsDual NSI equivalent (PC23, 103377-191/-449/-500, PD222400024-009, 2-8001140-1, 852420-XX)

Low-shock separation nut for constellation-class satellites of typically 500-1000 kg, qualified per AIAA S-113-2005.

Deployers & Separation Systems

Separation Nut PSM 3/8B

Beyond Gravity (ex-RUAG Space)

Price on request

Target spacecraft classOneWeb class satellites, typically 100-200 kg
QualificationAIAA S-113-2005 (former DOD-E-83578A)
InitiatorsDual NSI equivalent (PC23, 103377-191/-449/-500, PD222400024-009, 2-8001140-1, 852420-XX)

Smallest low-shock separation nut of the family, developed to fit OneWeb-class satellites of typically 100-200 kg.

Deployers & Separation Systems

PAS 432S (17 in) Separation System

Beyond Gravity (ex-RUAG Space)

Price on request

Interface diameter432 mm (17 in)
First applicationSatellites up to 200 kg at 0.45 mm on the VEGA launch vehicle
Release mechanismCBOD-LT Separation System Release Mechanism

Low-shock clamp band separation system designed for satellites up to 200 kg at 0.45 mm on the VEGA…

Deployers & Separation Systems

PAS 610S (24 in) Separation System

Beyond Gravity (ex-RUAG Space)

Price on request

Interface diameter610 mm (24 in)
CompatibilityMoog CSA ESPA; ESPA Rideshare User's Guide environments
Release mechanismCBOD-LT Separation System Release Mechanism

Low-shock separation system whose load capability is fully compatible with the Moog CSA ESPA and the ESPA Rideshare…

Deployers & Separation Systems

ESPA Separation System (PSR 1575 mm / 62 in)

Beyond Gravity (ex-RUAG Space)

Price on request

Interface diameter1575 mm (62 in)
CompatibilityEELV Secondary Payload Adapter (ESPA)
Release mechanismCBOD Low Shock Release Mechanism

1575 mm (62 in) low-shock clamp band separation system fully compatible with the EELV Secondary Payload Adapter (ESPA).

Deployers & Separation Systems

PAS 381S (15 in) Separation System

Beyond Gravity (ex-RUAG Space)

Price on request

InterfaceESPA 15 in adapter interface
Release mechanismCBOD-LT Separation System Release Mechanism
Scope of supplyLow shock clamp band separation system, interface rings, umbilical connection, separation spring set

Smallest member of the low-shock separation system family, developed to fit the ESPA 15 inch adapter interface.

Adapters & Rings

Modular Payload Adapter Systems

Beyond Gravity (ex-RUAG Space)

Price on request

MaterialsAluminium or carbon fibre composites
Launch vehicle compatibilityAlpha, Antares, Ariane, Atlas, Delta, Falcon 9/Heavy, New Glenn, Vega C, Vulcan
Separation recordMore than 1200 in-orbit separations, 100% success rate

Modular aluminium or carbon-fibre payload adapters compatible with Alpha, Antares, Ariane, Atlas, Delta, Falcon 9/H, New Glenn, Vega…

CubeSat Deployers

Satellite Dispenser Systems

Beyond Gravity (ex-RUAG Space)

Price on request

Subsystems includedStructure, separation system, electrical harness, thermal subsystem
Launch vehicle interfaceDispenser structure bolted to the launch vehicle upper stage
ReleaseSeparation nuts and spring units at each separation node

Multi-satellite dispenser systems combining structure, separation, harness and thermal subsystems, flown on Galileo, Radarsat Constellation and Eutelsat OneWeb.