The International Mars Prospecting Ride-Share System (IMPRESS) is presented here as a scalable, democratized, and low-cost mission architecture for distributed measurements on the martian surface and in the shallow subsurface. IMPRESS is intended to prospect on Mars in advance of sample return and human exploration. Its primary objective is to survey Mars for extant life, but it also supports geophysical, soil chemistry, resource, and landing-site risk assessments. Instead of relying on soft landers and drilling systems, IMPRESS deploys swarms of planetary penetrators that use descent kinetic energy to emplace instruments 0.2–1 m below the surface. This architecture provides spatial coverage, measurement replication, and mission redundancy. This increases the chance of detecting unevenly distributed biosignatures and gives negative results stronger context. Small penetrator platforms with standardized design, power, and communication interfaces lower the cost per experiment. The probes operate as independent nodes within a network, which enables time-correlated atmospheric, seismic, and environmental measurements that support the broader Mars exploration campaign. Repeatable mission deployments can range from small rideshare implementations with tens of penetrators to larger dedicated campaigns with hundreds or more. We describe the IMPRESS mission architecture, penetrator platforms, compatible payload classes, and how distributed shallow-subsurface surveys reduce scientific and operational uncertainty before future Mars surface activities. Key Words: Planetary penetrators—Mars—Extant life—Planetary protection—Distributed exploration—Rideshare. Astrobiology, 26, 688–699.
Hardware released during spacecraft entry can generate hypervelocity impacts that provide unique constraints on planetary subsurface properties. During NASA's Perseverance descent, two tungsten cruise ballast mass devices (CBMD) and fragments of the cruise stage formed meter‐scale craters north‐west of Jezero crater, i...
A. Sokołowska, I. Daubar, G. S. Collins et al.· Geophysical Research Letters· 0 citations
NASA launched the Mars Climate Orbiter and Mars Polar Lander in the late 1990s. Both missions failed because of critical yet preventable errors in testing and communication. The MCO was lost due to a unit conversion error between metric and imperial measurements, while the MPL likely failed because of an early engine s...
Fnu Abdullah· North Texas Journal of Under...· 0 citations
Project CERES proposes a reusable deep-space transportation architecture centered on the dwarf planet Ceres, combining nuclear thermal propulsion (NTP) with in-situ production of water, hydrogen, oxygen and ammonia. Its first flight, a Pathfinder that surveys Ceres and returns samples, also bears on the question of lif...
Lunar pits, some of which are interpreted as collapse features into underlying lava tubes, expose otherwise inaccessible stratigraphy and may provide entry points to subsurface voids that preserve records of lunar volcanism and offer potential sites for future human exploration. We synthesize the current state of knowl...
A. Mittelholz, S. Stähler, V. Bickel et al.· 0 citations
Lunar lava tubes have emerged as high-priority targets for future exploration and habitation due to their potential to
shield astronauts from radiation, thermal extremes, and micrometeorite impacts. This paper reviews current and emerging
methods for detecting subsurface cavities on the Moon, spanning gravimetric anoma...
O. C., Ozoadibe C., N. B. et al.· International Journal of Inn...· 0 citations
Fifty years of lunar drilling—three crewed campaigns and a succession of robotic missions from Luna 24 to Chang’e-6—has converged on a consistent pattern: no coring architecture has yet preserved the uppermost stratigraphic interval intact while reaching multi-meter depth safely. The Apollo record, through the lens of...
Ke Wang, Shao-Kun Wang, Dong Guo et al.· The Innovation Reviews· 0 citations
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