s p a c e f l i g h t s o l u t i o n s- HILTOP, Space, Exploration, Heliocentric

Nuclear or solar electric propulsion modeling
Comprehensive spacecraft and propulsion system models supports detailed system design
Heliocentric missions with up to 10 legs
Intermediate target encounters may be planetary swingbys or comet/asteroid flybys
Optional high-thrust capture at final target
Optional low-thrust escape from launch planet and/or capture at final target
Either launch vehicle dependent (LVD) or launch vehicle independent (LVI) launch modes
Final target may be a general heliocentric orbit
Interfaces to the JPL Dastcom3 file of 500,000+ asteroids and comets (recent copy included)
Interfaces with the JPL DE405 planetary ephemeris (copy included)
Supports development, maintenance and use of multiple User Defined Body ephemeris files
Compatibility with MAnE's Mission Builder utility program facilitates identification of multiple target missions
Draws ecliptic projection flight profiles instantly
Creates 20+ output files designed for presentation and analysis of mission data