Laboratoire Reaction Dynamics Inc.: federal grants and contributions: 8 agreements; $1.1M value; 2 departments; 6 programs.
Assay record ASY-CA-18UX1G517R · Cite as: Assay Systems, “Laboratoire Reaction Dynamics Inc.: federal grants and contributions”, https://assay-systems.com/register/ca/grants/r/laboratoire-reaction-dynamics-inc/
Germany ZIM – GNOMIC - Develop a modular Guidance and Navigation subsystem for launchers using F-prime OS and a Liquid Injection Thrust Vector Control (LITVC) engine control system.
Launching satellites is an expensive and unreliable process, yet demand for microsat launch services increases year after year. Reaction Dynamics is pioneering a revolutionary, inherently safe type of propulsion system. This technology demonstration aims to develop the competencies necessary to use hybrid rocket engines in launch vehicles, and build and operate launch vehicles reliably. Additionally, other systems for supporting space launch operations, such as ground infrastructure, supply chains, avionics and communication systems, will be developed. Within this proposal, Reaction Dynamics
This project comprises the development of a composite material overwrapped pressure vessel. The pressure vessel is intended for use in a rocket engine’s oxidizer feed system.
The funding provided from the Innovation Assistance Program is to assist innovative, early-stage small- and medium-sized enterprises that are unable to access existing COVID-19 business support.
The funding provided from the IAP program is to assist innovative, early-stage small- and medium-sized enterprises that are unable to access existing COVID-19 business support.
Development of hybrid rocket engine technology and the creation of a first working prototype for the micro satellite launcher market.
The funding provided from the Innovation Assistance Program is to assist innovative, early-stage small- and medium-sized enterprises that are unable to access existing COVID-19 business support.
Development and testing of a light composite combustion chamber and a refractory alloy nozzle extension for an hybrid rocket engine.
Contains information licensed under the Open Government Licence – Canada. Source: Government of Canada proactive disclosure of grants and contributions (open.canada.ca, dataset 432527ab-7aac-45b5-81d6-7597107a7013), 1,327,352 rows as published, collapsed to one agreement per agreement number (per reference number where none is given) at its latest amendment, which carries the full agreement value. Years are the agreement start year. Agreements with individuals are counted but not named.