Triton Aerogravity Assist Using a Flight-Proven, Inflatable Aerobrake for Neptune Orbit Capture

TL;DR

This paper explores using a flight-proven inflatable aeroshell for aerogravity assist at Triton, enabling Neptune orbit capture through numerical simulations of atmospheric entry at various velocities and angles.

Contribution

It introduces the use of the LOFTID inflatable aeroshell for aerogravity assist, extending prior work with a flight-proven technology for Neptune orbit capture.

Findings

Successful simulation of atmospheric entry at various velocities and angles.

Vehicle can reach Neptune orbit without exceeding thermal limits.

No lift generated due to zero angle of attack.

Abstract

Previous work by our group has shown the potential for an aerogravity assist at Triton using a trailing ballute to capture a probe into orbit about Neptune. The current work extends that study by using the LOFTID aeroshell configuration, a flight-proven inflatable, to perform the aeromaneuver. Numerical simulations were carried out beginning at the atmospheric interface for a range of entry velocities (3.0-14.0 km/s) and angles (45-56 degrees). The spin-stabilized vehicle was assumed to fly at zero angle of attack, producing no lift, and is capable of reaching outbound conditions sufficient to capture into orbit about Neptune without violating the vehicle's aerothermal limits or penetrating too deeply into Triton's atmosphere.