ADVANCED AND UNCONVENTIONAL EARTH-TO-ORBIT TRANSPORTATION CONCEPTS Robert H. Frisbee Soon to be Retired Jet Propulsion Laboratory As of 9-25-09, Home contact info: 4837 Alminar Ave., La Canada CA 91011 (818) 790-0508, FAX (818) 790-9678
[email protected] Presented at the Advanced Earth-to-Orbit Transportation Workshop National Institute of Aerospace Hampton VA 23667 September 3, 2009 OUTLINE • Introduction to the Problem • Focus Categories • Increasing Isp • Reducing system mass • Breakthrough physics • Reducing system costs • Evolutionary (incremental) versus Revolutionary • Infrastructure-Rich Systems • Beamed Energy (Laser, Microwave) • Launch Assist Catapults • Non-Propulsive (Tethers, Skyhooks, Towers) • Breakthrough Physics • Minimal-Infrastructure Systems • Advanced High Energy Density Matter (HEDM) Chemical • Nuclear • Aerial refueling • Summary and Recommendations 1 Introduction THE PROBLEM: LAUNCH COSTS > $10,000/kg GOAL: Reduce Costs Examples from the 1990s 2 Introduction THE PROBLEM: MISSION CAPABILITY GOAL: Enable New / Impossible Missions Mission V vs Propulsion Energy Density Mb /Mo = EXP( –V/Vex ) = EXP( –V/Isp ) You Are Here 2 2 3 2 E = M Vex = M Isp Introduction THE PROBLEM: NEED ADVANCED PROPULSION TECHNOLOGY BUT - IT TAKES TAKES TIME AND $$$ • Typically takes decades to go from concept to flight • Basic research often tied to grad student life cycle (e.g., 4+ years) • Costs dramatically increase over development life • $100K for "paper" studies, basic research -> $100M for space flight demo • Flight demos (e.g., New