Suborbital Reusable Vehicle Flight Tests

The rocket is a 2 stage, solid fuel, assembled aluminum body. It stands approximately 12 feet long, weighing 50 lbs at launch. During flight, it will reach Mach 5.5 on ascent, reaching a maximum altitude of 120 kilometers. It carries an electronic payload with a GPS-based telemetry system for airborne location tracking to collect data for flight trajectory analysis and motor characterization. We will also collect temperature data inside the payload bay for thermal analysis and capture inflight video. The vehicle is designed with Anvil to be highly reusable, with a marginal relaunch costs.