Green, Compact Hybrids for Nanosatellite Launchers

Low cost access to space is essential for continued commercial exploitation of near-earth environments, and to support future science missions. A serious limitation on the cost of space access is the available propellants and propulsion system technologies for launch, orbital insertion, maneuvering and orbital reinsertion, and reaction and attitude control.This Phase I STTR program will validate ignition and performance parameters for a volumetrically-optimized, low cost, green, shippable hybrid propellant motor for low cost access to space. The program is specifically targeted at validating performance via fabrication and delivery of replacements for the current Nihka and PSRM-120 stages (stage 2 and 3) based on the Black Brandt sounding rocket vehicle testbed under the Nanolaunch 1200 program guidelines.