Splashdown
Splashdown is the process of landing a spacecraft in an ocean, typically using a series of parachutes to decelerate the vehicle from reentry speeds of approximately 17,500 mph to a safe impact velocity of around 15 mph.[1] This method enables precise targeting of recovery zones across vast oceanic areas and allows for swift retrieval of the crew and capsule by specialized naval vessels and aircraft.[1] It has served as the primary recovery technique for United States crewed space missions since the inception of Project Mercury in 1961, encompassing suborbital and orbital flights, lunar landings, space station expeditions, and international collaborations.[2] The technique originated with NASA's Mercury program, where capsules were designed to splash down in the ocean for recovery by ship, beginning with Alan Shepard's suborbital flight on May 5, 1961, in the North Atlantic Ocean aboard Freedom 7.[2][1] It was refined during the Gemini and Apollo programs, supporting the Apollo program's lunar missions, including its six successful Moon landings, that splashed down primarily in the Pacific and Atlantic Oceans, with the Apollo-Soyuz Test Project in 1975 marking the final such recovery until the Space Shuttle era emphasized runway landings.[1] Splashdowns were reintroduced for crewed operations in 2020 through NASA's Commercial Crew Program, with SpaceX's Crew Dragon capsule completing its first astronaut return during the Demo-2 mission in the Gulf of Mexico off Florida's coast.[1] Subsequent missions, including Crew-9 and Crew-10 in 2025, have utilized splashdown sites off both Florida and California, demonstrating flexibility in Pacific and Atlantic recoveries.[3][4] Looking ahead, splashdown remains integral to NASA's Artemis program, as evidenced by the successful uncrewed recovery of the Orion spacecraft during Artemis I on December 11, 2022, in the Pacific Ocean west of Baja California.[5] The method's advantages include global accessibility for varying mission trajectories and established protocols for crew extraction within hours, often involving U.S. Navy divers and helicopters to address post-splashdown hazards like saltwater exposure or capsule instability.[1][6] While effective, it requires meticulous planning to mitigate risks such as inclement weather, structural integrity during deceleration, and environmental factors like biofouling on recovered hardware.[1]Definition and Procedure
Overview
Splashdown is the method of recovering a spacecraft, particularly re-entry capsules from orbital or suborbital missions, through a controlled descent and landing in a body of water, typically an ocean, where parachutes decelerate the vehicle to a safe impact velocity.[7][8] This approach originated with NASA's Project Mercury program in the early 1960s.[9] The process begins with atmospheric re-entry, where the spacecraft, traveling at speeds up to 25,000 mph (40,000 km/h) for lunar returns or about 17,500 mph (28,000 km/h) for low Earth orbit missions, encounters intense friction that generates temperatures up to 5,000°F (2,760°C) for high-energy re-entries.[8][7] To protect the crew and payload, ablative heat shields—composed of materials like Avcoat that vaporize to dissipate heat—are employed on the vehicle's base.[8] Following re-entry, a sequence of parachutes deploys: drogue parachutes first stabilize and reduce speed from around 325 mph (523 km/h), followed by main parachutes that further slow the descent to approximately 20 mph (32 km/h) for splashdown. Procedures vary by spacecraft; for example, NASA's Orion uses three main parachutes, while SpaceX's Crew Dragon employs four.[8][7] Post-impact, flotation devices such as airbags or floats may deploy to maintain upright orientation.[8] Ocean landings are selected over terrestrial sites because water covers about 70% of Earth's surface, offering a vast target area that accommodates trajectory uncertainties, while its low density and viscosity provide natural cushioning to absorb impact forces without requiring additional braking systems like retro-rockets.[7][10] Primarily conducted in the Atlantic and Pacific Oceans, splashdown operations involve coordination with naval forces, including the U.S. Navy and Coast Guard, to establish safety zones and deploy recovery vessels and helicopters for prompt crew extraction.[11][7] Common sites include areas off Florida's coast in the Atlantic or near San Diego in the Pacific.[11][8]Recovery Operations
Upon splashdown, the spacecraft activates a series of recovery aids to facilitate rapid location by recovery teams. These include radio beacons transmitting on VHF frequencies, flashing strobe lights, and deployment of sea dye markers to create a visible green patch on the water surface, aiding visual acquisition from aircraft or ships.[12][13] Modern systems, such as the Advanced Next-Generation Emergency Locator (ANGEL) beacons worn by astronauts, utilize the international Cospas-Sarsat satellite network operating at 406 MHz to provide precise location data within approximately 100 meters.[14] Recovery teams employ helicopters for aerial surveys, ships equipped with radar and sonar for tracking, and fast boats to close in on the signal.[11][15] Recovery equipment centers on specialized vessels and personnel trained for ocean operations. Primary recovery ships, often U.S. Navy amphibious assault vessels like the USS San Diego, feature well decks that allow smaller boats to launch and retrieve the capsule by winching it aboard using cranes and tending lines.[15] Helicopters, such as U.S. Air Force HH-60 Pave Hawk models, conduct initial surveys and deploy pararescue teams, while swimmer divers—typically Navy SEALs or Underwater Demolition Team specialists—approach the capsule to secure stabilization collars, inflatable platforms, and hoist lines for crew extraction and capsule retrieval.[11][16] For SpaceX Crew Dragon missions, dedicated recovery ships hoist the capsule directly onto the deck, with support boats checking for structural integrity and recovering parachutes.[11] Safety protocols prioritize crew health, vehicle integrity, and environmental protection. Divers and teams receive clearance from the NASA Recovery Director before approaching, and a 10-nautical-mile safety zone is enforced in coordination with the U.S. Coast Guard to manage maritime traffic.[11][15] Decontamination procedures address potential leaks of toxic hypergolic fuels like hydrazine and nitrogen tetroxide from reaction control systems, with teams in protective suits inspecting and neutralizing residues to prevent exposure; medical personnel perform immediate health checks on crew members post-egress.[11][17] Environmental measures include monitoring for fuel spills to mitigate water contamination, alongside recovery of hardware like parachutes to minimize ocean debris.[18] International and inter-agency coordination ensures seamless operations, particularly for multinational missions. NASA collaborates with the U.S. Navy, Air Force, and Coast Guard for American splashdowns, while joint efforts with partners like Roscosmos involve shared protocols for crew returns from the International Space Station, where U.S. vehicles handle splashdowns despite primary land-based recoveries for Soyuz capsules.[11][15] Procedures are validated through underway recovery tests, integrating equipment from contractors like Lockheed Martin and SpaceX.[14]Historical Development
Early Experiments
The development of splashdown techniques began in the late 1950s with U.S. military-led experiments to validate parachute systems and water recovery for spacecraft capsules. The U.S. Air Force and Navy conducted balloon and rocket drop tests using boilerplate mockups, dropping full-scale capsules from C-130 aircraft and helicopters to assess parachute deployment, free-fall stability, and initial water impact dynamics offshore Wallops Island, Virginia.[19] These pre-Mercury efforts, starting in October 1958 at NASA's Langley Research Center, involved numerous drops to refine extraction from aircraft, shock attenuation from parachute opening, and basic retrieval operations in ocean conditions.[19] The tests confirmed the feasibility of ocean landings but highlighted needs for improved flotation and righting mechanisms. As Project Mercury progressed from 1959 to 1963, suborbital and orbital qualification flights incorporated splashdown recoveries to verify end-to-end procedures. Uncrewed Little Joe rocket tests, such as Little Joe 1 in August 1959, evaluated launch escape systems followed by parachute descent and water impact, with recoveries demonstrating capsule stability under simulated abort scenarios.[20] A pivotal suborbital test occurred on January 31, 1961, with Mercury-Redstone 2 (MR-2), carrying chimpanzee Ham to an altitude of 157 miles and speeds up to 5,857 mph; the capsule splashed down in the Atlantic Ocean 422 miles downrange, 60 miles from the recovery ship, and was retrieved several hours later by helicopter despite minor leaks, validating biological tolerance and recovery protocols.[21] Orbital tests, including Mercury-Atlas 6 in February 1962, further refined splashdown accuracy, with the capsule landing within 4 miles of the target and recovered by USS Donner using frogmen and divers.[22] Soviet efforts in the late 1950s paralleled U.S. work through Vostok program simulations, prioritizing terrestrial landings for operational missions while exploring water recovery options under Sergei Korolev's OKB-1 design bureau for potential circumlunar applications.[23] These experiments focused on unmanned prototypes to mitigate risks from the spherical capsule's offset center of gravity during descent. Key challenges in these early experiments centered on capsule stability amid ocean waves, saltwater corrosion exposure, and coordinated recovery drills. Stability tests revealed that initial designs submerged the cylindrical section in winds up to 18 knots, prompting heat shield extensions and weight redistributions for better flotation and self-righting within 30 seconds of impact.[20] Saltwater immersion posed corrosion risks to ablative heat shields like nylon phenolic resin and René 41 afterbody shingles, necessitating post-recovery inspections and coatings to prevent degradation after prolonged flotation.[22] Recovery drills, involving Navy ships, helicopters, and sea-marker dyes, addressed imprecise splashdown zones spanning thousands of square miles, with boilerplate drops confirming landing bag inflation to soften impacts and maintain upright orientation for egress.[22]Key Milestones in Crewed and Uncrewed Missions
The Gemini program marked an early milestone in operational splashdown testing for uncrewed missions, with Gemini 2 conducting a suborbital re-entry flight in January 1965 that successfully demonstrated the spacecraft's heat shield and parachute recovery system upon ocean impact, paving the way for subsequent crewed flights. In 1966, additional uncrewed re-entry tests refined these procedures, contributing to the program's transition from experimental to routine Earth-orbit operations.[24] The Apollo program's lunar missions from 1968 to 1972 established splashdown as the standard recovery method for returning crews from deep space, with Apollo 11 achieving the first successful lunar sample return splashdown in July 1969 after a mission duration of over eight days.[25] Subsequent Apollo flights, including Apollo 12 and Apollo 15, utilized precision-guided re-entries to ensure accurate Pacific Ocean touchdowns, enabling the safe recovery of moon rocks and equipment.[26] The Skylab missions in 1973 and 1974 extended this approach to long-duration orbital stays, with each crew—Skylab 2 after 28 days, Skylab 3 after 59 days, and Skylab 4 after 84 days—completing record-setting flights via controlled splashdowns that tested human endurance limits.[27][28] The Apollo-Soyuz Test Project in July 1975 marked the final U.S. crewed splashdown before the Shuttle era, with the joint U.S.-Soviet mission recovered in the Pacific Ocean.[29] During the Space Shuttle era from 1981 to 2011, NASA shifted away from splashdowns for crewed returns, opting instead for runway landings to allow reusable orbiter operations and more flexible mission profiles, as the winged design enabled glider-like descents on concrete strips.[30] The program's retirement in 2011, after the final STS-135 mission, ended this runway-based approach and prompted a return to capsule-style recoveries, initially relying on international partners like Russia's Soyuz for International Space Station crew transport.[31] Post-Shuttle transitions revitalized splashdown reliance through NASA's Commercial Crew Program, with SpaceX's Crew Dragon capsule achieving its first operational crewed splashdown in 2020, marking the end of a 45-year gap in U.S. ocean recoveries and enabling routine ISS crew rotations.[32] For uncrewed applications, missions like SpaceX's Cargo Dragon resupply flights to the ISS have incorporated splashdowns since the 2010s, returning scientific payloads and experiments via ocean parachute descents.[33] Soviet uncrewed Zond missions in the late 1960s demonstrated splashdown recoveries for circumlunar flights, such as Zond 5 in 1968, which splashed down in the Indian Ocean after carrying tortoises and other biological specimens.[34] These evolutions underscored splashdown's adaptability across program shifts, from lunar exploration to commercial orbital logistics.Advantages and Challenges
Benefits
Splashdown offers significant targeting flexibility due to the vast expanse of the world's oceans, which cover approximately 70% of Earth's surface and provide a much larger landing area than constrained runway or terrestrial sites. This reduces the precision required for reentry trajectories, allowing for safer margins in case of minor deviations and enabling the selection of recovery zones based on launch profiles, such as those from equatorial sites that facilitate global ocean placements in international waters.[7] The water medium provides effective cushioning during impact, decelerating the spacecraft more gently than a hard landing on land and minimizing peak G-forces experienced by the crew, typically in the range of 4 to 6 g during final descent and splashdown. This is lower than the forces associated with unassisted terrestrial impacts, which can exceed 10 g without additional braking systems, thereby reducing the risk of injury and structural damage.[35][25] Logistically, splashdown sites can be positioned close to major launch facilities, such as the Atlantic Ocean zones near Cape Canaveral, allowing for rapid recovery using ships and helicopters already stationed in proximity. Operations in international waters simplify coordination by avoiding overland territorial issues and leveraging established naval support, as outlined in NASA recovery protocols.[30][36] From a cost perspective, the simpler capsule design required for splashdown—relying on parachutes rather than complex landing gear or wings—lowers overall development and operational expenses while facilitating reusability through easier refurbishment of recovered vehicles. For instance, SpaceX's Crew Dragon capsules have demonstrated multiple successful post-splashdown inspections and reflights, contributing to reduced mission costs in commercial programs.[30][37]Limitations and Risks
Splashdown recoveries are highly susceptible to adverse weather conditions, such as high winds, rough seas, and typhoons, which can delay operations and necessitate mission extensions or site relocations to ensure safe retrieval of the spacecraft and crew. For instance, NASA's SpaceX Crew-4 mission departure from the International Space Station was postponed in October 2022 due to unfavorable weather forecasts at the planned splashdown zones off Florida's coast, with teams conducting repeated reviews to assess sea state and wind conditions. Similarly, the Crew-8 return in October 2024 faced multiple delays from elevated winds and waves exceeding operational limits, extending the mission by weeks and highlighting the need for flexible scheduling in ocean-based landings. The Crew-10 mission in August 2025 also experienced delays due to unfavorable weather conditions off the California coast. Historical missions like Apollo 13 also contended with weather variability during reentry planning, where initial Pacific Ocean site forecasts influenced trajectory adjustments to avoid marginal conditions, though the final splashdown occurred under acceptable visibility and wave heights.[38][3] Environmental hazards from splashdown include the potential release of toxic propellants, particularly hydrazine used in reaction control systems, which can contaminate ocean waters and pose risks to marine ecosystems. Hydrazine is a highly toxic, carcinogenic substance that causes severe chemical burns on contact and persists in aquatic environments, potentially disrupting marine life through bioaccumulation in food chains. NASA environmental impact statements for programs like the Space Shuttle and Constellation have quantified increased use of such hypergolic fuels, noting their fourfold toxicity compared to alternatives and the challenges in containing spills during post-landing handling. In crewed capsules like Orion, residual hydrazine onboard after reentry could leak during recovery, exacerbating local pollution, as assessed in risk analyses for warm ocean areas where dispersal might affect fisheries and wildlife. Mitigation strategies involve pre-splashdown propellant venting where feasible and rapid containment by recovery teams to minimize ecological disruption.[39][40] Crew safety during ocean splashdown carries specific risks, including drowning from capsule instability in currents, hypothermia in colder waters, and the need for prompt medical evacuations post-immersion. Capsules may land in an unstable orientation, such as upside down, complicating egress and increasing drowning hazards if hatches fail to open quickly or if waves flood the interior, particularly for deconditioned astronauts after long-duration flights. In cooler recovery zones, prolonged exposure to water temperatures below 20°C (68°F) can induce hypothermia within minutes, impairing crew mobility and consciousness despite pressure suits' insulation, as detailed in NASA's post-landing survival assessments for vehicles like Orion. Medical evacuations have been required in cases of disorientation or injury during extraction, with helicopter transfers to ships mitigating these threats but adding procedural complexity. To counter these, designs incorporate flotation devices and righting bags, while recovery protocols prioritize swift swimmer-assisted egress.[41][42] Logistically, splashdown demands substantial naval resources, including aircraft carriers, amphibious assault ships, and support vessels, which incur high operational costs and coordination challenges. U.S. Navy involvement, as seen in recoveries for Apollo and modern Commercial Crew missions, mobilizes thousands of personnel and specialized equipment like cranes and divers, with estimates placing single-mission recovery expenses in the millions due to fuel, maintenance, and deployment logistics. For example, exercises for Orion recovery on ships like USS John P. Murtha demonstrate the scale, involving extensive training and at-sea positioning that strain military budgets. Geopolitical considerations arise in international recovery zones, where operations in open ocean areas require adherence to treaties and can face interference from foreign vessels, prompting enhanced security patrols by the U.S. Coast Guard to protect assets and ensure unimpeded access. These factors contribute to ongoing efforts to transition toward more autonomous or land-based alternatives to reduce dependency on naval infrastructure.[43][44]Spacecraft and Vehicles
Crewed Spacecraft Designs
Crewed spacecraft designed for splashdown typically feature compact, blunt-body capsules to withstand atmospheric re-entry and ensure stable water landings. These designs prioritize human safety through robust thermal protection, controlled descent, and post-impact stability, drawing from early programs like Project Mercury and Apollo. The capsules are engineered to float upright or with minimal tilt, allowing for rapid crew egress and recovery while minimizing risks such as capsizing or submersion. The predominant shape for crewed splashdown capsules is a conical or bell-like form, which provides aerodynamic stability during re-entry and helps maintain balance on water. For instance, the Apollo Command Module (CM) employed a blunt cone with an offset center of gravity—achieved by positioning heavier components like the propulsion system lower—to ensure it naturally rights itself after splashdown, reducing the likelihood of inversion. This configuration, tested extensively in wind tunnels and drop tests, allowed the capsule to settle with its base down, facilitating hatch access for the crew. Similar principles inform modern designs, where the capsule's geometry is optimized to minimize hydrodynamic drag and promote positive buoyancy. Re-entry systems in these spacecraft emphasize ablative heat shields and multi-stage parachutes to manage deceleration and protect occupants from peak heating. The Apollo CM used Avcoat, a phenolic epoxy resin that ablates during re-entry to dissipate heat, with a thickness of about 0.5 inches covering the conical forward section; this material choice enabled survival of temperatures exceeding 2,500°C while keeping the crew compartment below 120°C. Descent is controlled by drogue parachutes for initial stabilization, followed by 2-5 main parachutes deployed sequentially to achieve a terminal velocity of approximately 30-35 feet per second (20-24 mph) at splashdown, balancing splash loads below 10g for crew tolerance. These features ensure precise targeting within a 10-20 nautical mile recovery zone. Post-splashdown flotation is enhanced by integrated aids that counteract any initial instability. Inflatable bags, often deployed from the capsule's apex or sides, provide additional buoyancy and torque to upright the vehicle if it lands at an angle greater than 20 degrees. The Apollo CM, for example, included four inflatable bags that could be remotely activated by recovery forces, while ballast release mechanisms—such as jettisoning temporary weights—further adjust the center of gravity for stability. Uprighting systems, like small thrusters or passive fins, are sometimes incorporated to orient the capsule within minutes, preventing prolonged exposure to waves. These mechanisms have been refined through simulations showing flotation times of up to 48 hours in rough seas. Early designs from Project Mercury influenced subsequent crewed capsules, establishing a heritage of reliable splashdown architecture. The Mercury capsule, a bell-shaped cone with a beryllium heat shield, used three main parachutes and flotation collar bags for stability, achieving successful water recoveries in all six crewed flights. This legacy persists in NASA's Orion spacecraft, which adapts Apollo-style offset gravity and Avcoat shielding for Artemis missions, with three main parachutes (tested including two-parachute contingencies to handle dynamic loads up to approximately 25,000 pounds).[45] SpaceX's Crew Dragon incorporates a similar conical form with PICA-X ablative material—derived from Stardust probe technology—and eight SuperDraco thrusters for powered descent adjustments, supplemented by four parachutes and deployable trunk fins for uprighting. Even Russia's Soyuz, primarily land-landing, includes water adaptations like a soft-landing engine cutoff override and flotation beacons for emergency splashdowns, as demonstrated in contingency planning for the International Space Station. These evolutions highlight a focus on redundancy and human-rated margins in splashdown-optimized designs.Uncrewed Spacecraft Applications
Splashdown has been employed in uncrewed missions primarily for the safe return of scientific samples and hardware from low Earth orbit, enabling the recovery of delicate payloads that would otherwise be lost in destructive re-entries. The SpaceX Cargo Dragon spacecraft, operating under NASA's Commercial Resupply Services program, exemplifies this application by utilizing parachute-assisted ocean landings to deliver up to 3,000 kg (6,614 pounds) of return cargo, including biological, physical, and materials science experiments conducted aboard the International Space Station (ISS).[46] This approach contrasts with land-based recoveries used in interplanetary sample returns, such as those from asteroids, by prioritizing water cushioning to minimize impact forces on sensitive payloads during uncrewed operations.[47] Notable examples include the CRS-25 mission in August 2022, where the uncrewed Dragon splashed down off Florida's coast, returning over 3,600 pounds (1,630 kg) of cargo, including human research samples, biotechnology studies, and cold storage units for biological specimens. Similarly, the CRS-17 mission in June 2019 recovered materials from ISS experiments via a controlled splashdown in the Pacific Ocean, demonstrating the reliability of this method for iterative science returns. These operations involve a deorbit burn followed by atmospheric re-entry, deployment of drogue and main parachutes, and recovery by NASA and SpaceX teams within hours to preserve sample integrity.[47][48] In deorbiting technologies for uncrewed spacecraft and defunct satellites, splashdown principles inform controlled re-entries targeting remote ocean areas to mitigate ground risks, though most lack parachutes and instead rely on freefall breakup for disposal. For instance, Northrop Grumman's Cygnus cargo vehicle, after completing ISS resupply missions, performs destructive re-entries over the Pacific Ocean, where the spacecraft fully disintegrates to prevent orbital debris without recoverable parachutes. This freefall distinction from parachute-equipped capsules like Dragon allows larger-scale disposal of uncrewed hardware—Cygnus can manage up to 8,000 pounds (3,600 kg) of waste—but precludes sample recovery. Smaller probes, such as experimental satellites with drag devices, may achieve partial control but rarely use parachutes for ocean splashdown due to size constraints and cost.[49][50] Payload protections in uncrewed splashdown capsules emphasize sealed compartments to shield geological, biological, or experimental samples from saltwater exposure, high deceleration, and post-landing contamination. In Cargo Dragon returns, samples are housed in robust, hermetically sealed containers—often with thermal insulation and vapor-tight seals—to maintain viability during the 18-24 hour recovery window, as seen in missions returning microbial cultures and protein crystal growth experiments. For potential future applications like Mars sample returns, NASA protocols incorporate multi-layered containment systems, including bio-containment vessels that isolate extraterrestrial materials to prevent forward or backward contamination, aligning with COSPAR planetary protection guidelines. These "bio-shields" ensure samples remain sterile externally while preserving internal integrity, adaptable to splashdown scenarios despite current Mars plans favoring land recovery. Scale variations highlight this: compact probes (e.g., under 100 kg like early sample capsules) use minimal shielding for targeted returns, while larger uncrewed vehicles like Dragon integrate modular sealed bays for diverse payloads exceeding 1 ton.[51][52]Notable Events and Records
Crewed Splashdowns
Crewed splashdowns represent a critical phase in human spaceflight, where spacecraft carrying astronauts descend into oceanic targets under parachutes, prioritizing crew safety through flotation devices and rapid recovery by naval or commercial vessels. These events have been integral to U.S. programs from Project Mercury through the Commercial Crew era, with recovery operations evolving from destroyer-based teams to specialized SpaceX ships equipped with cranes and medical support. The following table summarizes key crewed splashdown events, highlighting mission specifics, landing parameters, and recovery details for representative milestones.| Mission | Date | Coordinates (approx.) | Recovery Ship | Miss Distance | Notable Issues |
|---|---|---|---|---|---|
| Mercury-Atlas 6 (Friendship 7) | February 20, 1962 | 21°18′N 64°20′W | USS Noa | 5 nautical miles | First U.S. orbital crewed flight; minor attitude control issues during reentry.[53] |
| Gemini 8 | March 17, 1966 | 25°07′N 136°00′E | USS Leonard F. Mason | 3 miles | Emergency abort due to thruster malfunction; rough seas complicated recovery, requiring flotation collar stabilization.[54][55] |
| Apollo 8 | December 27, 1968 | 8°08′N 165°01′W | USS Yorktown | 2.9 miles | Successful return from first crewed lunar orbit mission; precise targeting after translunar injection.[56] |
| Apollo 13 | April 17, 1970 | 21°38′S 165°22′W | USS Iwo Jima | 3 nautical miles | Aborted lunar landing due to service module explosion; crew survived in lunar module, with trajectory adjustments causing drift from planned site.[57] |
| Skylab 4 | February 8, 1974 | 31°18′N 119°48′W | USS New Orleans | 3 miles | Record duration of 84 days; minor guidance tweaks for Pacific targeting after extended station operations.[58] |
| Crew Dragon Demo-2 | August 2, 2020 | 29°50′N 87°00′W | GO Navigator (SpaceX) | <1 km | First NASA-certified commercial crew return; smooth reentry with integrated SuperDraco abort system readiness. |
| Crew-8 | October 25, 2024 | 30°00′N 87°30′W | MV Megan (SpaceX) | <1 km | Delayed undocking due to weather; successful six-month ISS rotation with four crew members.[59] |
| Crew-9 | March 18, 2025 | 29°30′N 84°00′W | SpaceX recovery vessel | <1 km | Return of NASA astronauts and Roscosmos cosmonaut after extended ISS mission; splashdown off Florida coast.[4] |
| Crew-10 | August 9, 2025 | 32°30′N 120°00′W | SpaceX recovery vessel | <1 km | First Commercial Crew Program splashdown in the Pacific Ocean off California; six-month ISS rotation.[3] |
Uncrewed Splashdowns
Uncrewed splashdowns represent a critical aspect of spacecraft testing and operations, enabling the validation of re-entry, descent, and recovery systems for future crewed missions while returning scientific data and hardware from orbit. These missions have evolved from early suborbital and orbital tests in the 1960s to contemporary cargo resupply flights and prototype demonstrations for deep space exploration. Key examples include NASA's Mercury program tests, which pioneered controlled water landings, and recent SpaceX Dragon capsule returns from the International Space Station (ISS).[60] The following table summarizes select uncrewed splashdown missions, highlighting their agencies, dates, locations, recovery methods, and outcomes related to payload integrity and mission objectives.| Mission | Agency | Date | Location/Coordinates | Recovery Method | Payload Success |
|---|---|---|---|---|---|
| Mercury-Atlas 4 | NASA | September 13, 1961 | Atlantic Ocean (approx. 30°07' N, 64°02' W) | Parachute descent; ship recovery by USS Donner | Successful; first U.S. uncrewed orbital flight, tested attitude control and re-entry systems. |
| Crew Dragon Demo-1 | SpaceX/NASA | March 8, 2019 | Atlantic Ocean (approx. 27°55' N, 73°53' W, off Florida coast) | Parachute descent; recovery by SpaceX ships (GO Quest, GO Navigator) | Successful; demonstrated autonomous docking to ISS and safe return for crewed certification.[61] |
| CRS-21 | SpaceX/NASA | January 14, 2021 | Gulf of Mexico (approx. 27°30' N, 82°30' W, west of Tampa) | Parachute descent; recovery by SpaceX ship (GO Navigator) | Successful; returned over 5,400 lbs of cargo, experiments, and hardware from ISS.[62] |
| Artemis I | NASA | December 11, 2022 | Pacific Ocean (approx. 29° N, 118° W, near Guadalupe Island off Baja California) | Parachute descent; recovery by USS Portland (LPD-27) | Successful; completed 25-day lunar orbit, tested Orion systems for future crewed Artemis missions. |
| Starship IFT-4 | SpaceX | June 6, 2024 | Indian Ocean (approx. 10° S, 70° E) | Controlled soft landing; no physical recovery | Successful; validated re-entry heat shield and propulsion for reusable architecture. |