May 5 – 9, 2025
STELLENBOSCH, CAPE TOWN, SOUTH AFRICA
Africa/Johannesburg timezone

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TERP RAPTOR (Terrapin Engineered Rideshare Probe for Rapid-response Asteroid Apophis Profiling, Tracking, Observing, and Reconnaissance): Mission Concept Development

May 6, 2025, 5:25 PM
8m
STELLENBOSCH, CAPE TOWN, SOUTH AFRICA

STELLENBOSCH, CAPE TOWN, SOUTH AFRICA

Protea Hotel by Marriott® Stellenbosch
Oral. Apophis T-4 Years Session 3: Apophis T-4 Years

Speaker

Adrienne Rudolph (University of Maryland)

Description

The $\sim$325-meter diameter Potentially Hazardous Asteroid (PHA) designated 99942 Apophis 2004 MN$_{\text{4}}$ will make a historic close approach of Earth on April 13th, 2029, passing within $\sim$31,634 km of Earth’s surface, $\sim$4,152 km closer than our geosynchronous satellites. This is an extraordinarily unique opportunity for collecting data on a several hundred-meter size asteroid while it experiences the effects of close proximity to Earth’s gravitational field. Current asteroid population models suggest that this is a 1 in 7500 years event. Apophis’s Earth close encounter therefore provides a rare opportunity to observe planetary encounter effects on an asteroid.

Our Terrapin Engineered Rideshare Probe for Rapid-response asteroid Apophis Profiling, Tracking, Observing, and Reconnaissance (TERP-RAPTOR) is an Earth-orbiting mission concept in which a 12U CubeSat built by University of Maryland students would perform a flyby of Apophis, collecting data to address science questions regarding the asteroid's collisional and dynamical evolution, its surface and structural characteristics, and the effects of close proximity to Earth's gravitational field. This mission also supports planetary defense objectives by advancing our understanding of Apophis-sized objects and their potential Earth impact risks.

The mission launches as a rideshare into an Apophis-intercepting orbit, an example of which is shown in Figure 1. We present several design reference mission cases, including an orbit potentially reachable from a typical Geosynchronous Orbit Transfer (GTO) rideshare launch, a high-inclination sub-geosynchronous altitude orbit with lower flyby speed and more benign radiation environment, and a retrograde orbit scenario minimizing flyby speed relative to Apophis but requiring advanced future launch rideshare systems, such as Blue Origin’s Blue Ring.

After launch and separation, TERP-RAPTOR performs on-orbit commissioning, loiters, and then maneuvers to fly by Apophis at its perigee. Data is collected by two cameras: a high-resolution RGB imager for wide-field analysis of asteroid size, shape, spectral weathering signatures, and crater distribution; and a multi-spectral imager with customizable bands (up to near-infrared) to detect fine-scale surface changes. TERP-RAPTOR will also carry an antenna instrument provided by the High-frequency Active Auroral Research Program (HAARP) and collect HAARP's bi-static radar signals reflected by Apophis, in collaboration with the Owens Valley Radio Observatory. Those data help characterize portions of Apophis's interior. Image data and HAARP data will be stored onboard and down-linked to ground stations.

The spacecraft may then perform extended missions. As the spacecraft nears the end of its operational lifetime, it will conduct End-of-Life operations adhering to NASA Procedural Requirements for Limiting Orbital Debris.

TERP-RAPTOR is an innovative design for a small, affordable University-built spacecraft capable of providing a higher ratio of scientific return to mission cost than any previous mission to an asteroid or comet. Apophis will be naked-eye visible in the night sky in parts of Europe and Africa, capturing the attention of everyone around the world. As people's eyes and imaginations gaze upwards, TERP-RAPTOR will be our eyes in space, alongside any other spacecraft that the nations of the world might dispatch to study this extraordinary natural event.

Author

Adrienne Rudolph (University of Maryland)

Co-authors

Brent Barbee (University of Maryland) Cameron Storey (University of Maryland) Chinthan Prasad (University of Maryland) Dr David Akin (University of Maryland) Jarred Young (University of Maryland) Joe Huba Kruti Bhingradiya (University of Maryland) Mark Haynes (NASA Jet Propulsion Laboratory) Dr Mary Bowden (University of Maryland) Dr Paul Bernhardt (University of Alaska) Rahul Vishnoi (University of Maryland) Ryan Mahon (University of Maryland) Sean Philips (University of Maryland) Yunghsin Chen

Presentation materials