Launch Vehicle Performance Optimization
AscendArc's trajectory optimization and launch vehicle performance software — maximizing payload delivery to orbit through advanced ascent guidance and staging algorithms.
Technical specifications
- Product
- Trajectory optimization software + flight GNC algorithms
- Capability
- Real-time ascent trajectory replanning (wind/performance deviations)
- Benefit
- Maximize payload-to-orbit per kg of propellant consumed
- Target Customers
- Commercial launch vehicle developers, rideshare satellite operators
- Technology
- Constrained optimization, real-time GNC, staging/separation timing
About
AscendArc develops trajectory optimization and launch vehicle flight software for the commercial launch industry. The company’s name reflects its core capability: optimizing the ‘arc’ that a launch vehicle follows as it ‘ascends’ from Earth’s surface to orbit — the trajectory that determines how much payload a given rocket can deliver to a specified orbit.
Trajectory optimization for launch vehicles is a computationally intensive problem involving constrained optimization over continuous dynamic systems — balancing gravity losses, aerodynamic drag, propellant consumption, staging events, fairing separation, and orbit injection accuracy across a multi-stage ascent. Even small improvements in trajectory algorithm efficiency can translate to hundreds of kilograms of additional payload capacity on a given mission.
AscendArc’s flight software for guidance, navigation, and control (GNC) implements real-time trajectory planning algorithms that can update the optimal ascent path mid-flight in response to wind disturbances, off-nominal performance, or range safety constraints. The company targets commercial launch vehicle developers (the growing NewSpace launch sector needs cost-efficient GNC software) and provides trajectory analysis as a service to satellite operators planning rideshare missions.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.