Green, Compact Hybrids for Nanosatellite Launchers

Period of Performance: 06/17/2015 - 06/17/2016

$125K

Phase 1 STTR

Recipient Firm

Terves Inc.
24112 Rockwell Drive Array
Euclid, OH 44117
Firm POC
Principal Investigator

Research Institution

Pennsylvania State University
110 Technology Center Building
University Park, PA 16802
Institution POC

Abstract

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.