Author:
Whitmore Stephen A,Stoddard Robb L
Reference47 articles.
1. Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets;Whitmore;Journal of Propulsion and Power,2015
2. Additively Manufactured Acrylonitrile-Butadiene-Styrene-Nitrous-Oxide Hybrid Rocket Motor with Electrostatic Igniter;Whitmore;J Propulsion Power,2015
3. Comparing Hydroxyl Terminated Polybutadiene and Acrylonitrile Butadiene Styrene as Hybrid Rocket Fuels;Whitmore;J Propulsion Power,2013
4. Whitmore SA. Additive Manufacturing as an Enabling Technology for "Green" Hybrid Spacecraft Propulsion. Conference on Recent Advances in Space Technology 2015: Istanbul, Turkey; 2015.
5. Whitmore SA, Merkley SL, Zachary S, et al. Development of a Power Efficient, Restartable, "Green" Propellant Thruster for Small Spacecraft and Satellites. SSC15-P-34, 29th AIAA/USU Conference on Small Satellites: Logan, UT; 2015.
Cited by
8 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献