SOW-ReactionWheelforDione.pdf
PDF 15 KB Posted
- Attached to
- Flight Model/Reaction Wheels Federal contract opportunity
- Solicitation number
- 80NSSC202342
View the file
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
STATEMENT OF WORK
1. Objective/Requirements
The purpose of this purchase is to acquire four reaction wheels to support attitude control for Dione, an in-house CubeSat mission.
2. Characteristics, Scope, and Specs
The procurement is specifically for:
Three (3) flight reaction wheels One (1) engineering model reaction wheel End Item Data Package for each reaction wheel, including (but not limited to):
o Test data o Photographs o Component documentation
All reaction wheels shall comply with the following characteristics:
Momentum storage capacity of at least 30 mNms Fits within a volume of 50mm x 50mm x 40mm Command and telemetry interface: I2C Operate properly with an input voltage of +5V Mass: no more than 190g Torque output: at least ±2 mNm above internal losses while storing ±20 mNms of angular momentum
In addition, flight reaction wheels shall comply with the following:
EEE parts from lots screened for radiation survivability Meet performance requirements with interface temperatures of -40°C to +70°C Survive interface vibration loads of at least 12 Grms Have on-orbit heritage (demonstrated on-orbit operation) Draw no more than 2W when operating in vacuum
3. Place of Performance
Vendor facility.
4. Period of Performance Delivery of all items maximum of 6 months after award of contract.
File details come from the government source that posted it. Updated .