Multiple User System for Earth Sensing Facility
Facility Description
MUSES was launched in June 2017, achieving Full Operating Capability in September 2017, and has been in continuous operations since that time. The facility accommodates up to four (two “large” and two “small”) robotically installed instruments referred to as “Hosted Payloads”, with inertial attitude estimation, and off-nadir pointing capability enabled by a dedicated inertial measurement unit, star tracker, two-axis gimbal system, and a dedicated Server hosted internally in the International Space Station US Laboratory.
The ISSInternational Space Station orbital inclination (51.6 deg) and MUSES pointing capability (5 deg ISS Starboard/45 deg ISS Port and +/- 25 deg ISS Forward/Aft) provide for a near-global coverage profile with capability up to 55 deg North and 52 deg South in latitude or around 90% of the inhabited Earth.
The MUSES pointing accuracy is better than 30 arc seconds, which corresponds to about 60 m on the ground at an ISS altitude of 400 km and the MUSES Master Time provided to hosted payloads has an accuracy of <±250 μsec to GPS time. Geo-location is sourced from the ISS GPS system and is accurate to ±50 m.
All Payload Accommodations include:
Test and integration support for MUSES and ISS
Launch (pressurized/soft-stowed) services
Robotic transfer/installation and return (if desired) services
Commanding through Gbit ethernet
Payload health and status via Gbit ethernet
Primary data transmitted via Gbit ethernet
Radiative heat rejection only. Heater Power available
Hosted Payload data file(s) transfer, downlink, and delivery
Large Payload Accommodations provide support equivalent to small satellite payloads in the 100 lb to 200 lb class.
Maximum Mass: 100 kg
Maximum Height: 35″ (92cm)
Maximum Width: ~18″ (~46 cm) diameter
Maximum Power: 222 W @ 28 Vdc
Small Payload Accommodations provide support equivalent to small satellite payloads in the 50 lb to 100 lb class.
Maximum Mass: 50 kg
Maximum Height: 35″ (92 cm)
Maximum Width: ~10″ (~25 cm) diameter
Maximum Power: 112 W @ 28 Vdc
Availability:The general availability status of the facility. Please contact the facility manager
ISS Environment:The facility location (internal or external to the ISS.) External
Owner:The entity that owns the facility. Teledyne Brown Engineering
Operator/Implementation Partner:The entity or ISS National Lab Implementation Partner that operates the facility.
Teledyne Brown Engineering
Developer(s):The entity, or entities, that developed the facility.
Teledyne Brown Engineering
Facility Manager:The name of the facility manager and their organization.
Heath Lester
Teledyne Brown Engineering
Manager Email:The facility manager's email address.
tbe_muses_ops@teledyne.com
Parent Facility:Any facility that is necessary to operate the facility described on this webpage. i.e., a parent facility is one level higher in the operational hierarachy. ELC
Child Facility:Facilities that can be operated within the facility described on this webpage.
Sponsoring Space Agency:The government space agency that sponsors investigations that use the facility. NASA
Equipment Category:"The facility's ISS National Lab equipment designation type. Designations include:
1. ISS National Lab Commercial Service Provider (CSP) Facility
2. Support Hardware
3. Capability ISS National Lab CSP Facility
Additional Information:Additional resources to learn more about the facility.
Teledyne Brown Engineering Geospatial Solutions
MUSES Overview
MUSES on NASA’s SSRE