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Demonstration Rocket for Agile Cislunar Operations

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(Redirected fromDemonstration Rocket for Agile Cislunar Operations (DRACO))
U.S. Space Nuclear Thermal Propulsion

DRACO
Representation of the rocket
FunctionSpacecraft
ManufacturerLockheed Martin
Country of originUnited States
Project cost$499 million (Phases 2 and 3)[1]
Launch history
StatusCancelled
Payloads
Payload tolow Earth orbit
Payload toMoon
Payload toVenus
Payload toMars
Stages information
First stage
Second stage

TheDemonstration Rocket for Agile Cislunar Operations (DRACO) was a planned spaceflight demonstration mission under the joint auspices of DARPA, NASA, Lockheed Martin, and BWX Technologies, aiming to carry out the first in-orbit test of anuclear thermal rocket by 2027.[2][3][4] Fuelled bylow-enriched uranium,[3][4][5] its reusability and performance were projected to significantly outpace current chemical propulsion systems. Launch operations were to be supported by theU.S. Space Force, with theVulcan Centaur rocket identified as the planned launch vehicle.[6] In 2023,NASA formally joined the DRACO program, seeking to leverage nuclear propulsion to drastically reduce travel time to deep-space destinations such asMars.[7] Nuclear thermal propulsion was expected to yield two to three times the efficiency ofchemical propulsion, with mission durations to Mars potentially cut in half.[8] DARPA program manager Tabitha Dodson remarked that nuclear propulsion could form the foundation for evolving systems such as fusion-based spacecraft, enabling more ambitious human exploration missions with greater safety margins.[9] According to Lockheed Martin and BWXT, there were considerable efficiency and time gains from the nuclear thermal propulsion.[10][11] NASA believed the much higher efficiency will be two to three times more than chemicalpropulsion,[6] and the nuclear thermal rocket is to cut the journey time to Mars in half.[12]

However, by January 2025, the mission's planned 2027 launch was placed on indefinite hold due to technical and regulatory challenges such as the complex safety and testing requirements for ground-based nuclear reactor validation and the unresolved final design of the propulsion system.[13][14] The program's status was further impacted by the May 2, 2025 release of the FY2026 federal budget, which proposed a $531 million cut to NASA’s Space Technology Mission Directorate. The budget documentation cited reductions in unspecified advanced space propulsion projects.[15] Some analysts interpreted this as effectively ending nuclear propulsion research, noting similarities to NASA’s earlier cancellation ofProject Prometheus.[14]

On May 30, 2025, the finalized FY2026 President's Budget Request confirmed DRACO's cancellation, with no funding allocated to nuclear thermal or electric propulsion programs, deemed by the Trump administration as expensive, and DARPA had completed its program termination procedures, transferring the knowledge to NASA.[16][14] In late June 2025, DARPA announced that the termination was based on an assessment that the costs no longer matched the benefits[17] and that decreasing launch costs and new analysis led to its cancellation.[18] Although the Senate Appropriations Committee has indicated a preference for maintaining current funding levels for NSF and NASA, resisting the Trump administration's proposed drastic cuts, which support suggests a potential safeguard for ongoing research and missions including other projects that might involve NTP and NEP, the cancellation of DRACO is final due to DARPA's withdrawal from it.

Background

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In May 1946, theU.S. Air Force launched theNuclear Energy for Propulsion of Aircraft (NEPA) project to explore the potential of nuclear energy for powering aircraft.[19][20] This initiative led to a collaborative effort of the Air Force and theU.S. Atomic Energy Commission (AEC) known as theAircraft Nuclear Propulsion (ANP) program, aimed at developing nuclear propulsion systems for aerospace vehicles.[19][20] The ANP Program was canceled in March 1961 after investing $1 billion.[19][20]

Using nuclear energy for space travel reportedly has also been discussed since the 1950s among industry experts.Freeman Dyson andTed Taylor, through their involvement inProject Orion, aimed to create an early demonstration of the technology. Ultimately, the project received backing fromWernher von Braun, and reached the test flight stage of development, but the project ended early due to environmental concerns.[21]

In 1955, the Air Force partnered with AEC to develop reactors for nuclear rockets underProject Rover.[22] In mid-1958, NASA replaced the Air Force[22] and built Kiwi reactors to test nuclear rocket principles in a non-flying nuclear engine.[23] With the next phase's Nuclear Engine for Rocket Vehicle Application (NERVA), NASA and AEC sought to develop a nuclear thermal rocket for "both long-range missions to Mars and as a possible upper-stage for theApollo Program."[23] Due to funding issues, NERVA ended in 1973 without aflight test.[23]

New program

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In 2020, theNational Academies of Sciences, Engineering, and Medicine, at the request of NASA, convened an ad hoc Space Nuclear Propulsion Technologies Committee to identify primary technical and programmatic challenges and risks for the development of space nuclear propulsion technologies for use in future exploration of theSolar System. With regard to nuclear thermal propulsion (NTP) systems, the committee identified the following technological challenges.[24]

  • A high operating power density and temperature of the reactor are necessary to heat the propellant to approximately 2700 K at the reactor exit for the duration of each burn.
  • The need for long-term storage and management of cryogenic, liquid hydrogen (LH2) propellant.
  • Short reactor startup times (as little as 60 s from zero to full power) relative to other space or terrestrial power reactors.
  • Dealing with the long startup and shutdown transients of an NTP system relative to chemical engines. This drives design of the engine turbopumps and thermal management of the reactor subsystem.

The committee also emphasized the lack of adequate ground-based test facilities, noting that "There are currently no facilities in the United States that could conduct a full-power ground test of a full-scale NTP reactor comparable to the Rover/NERVA experiments."[24] Nevertheless, the committee's report concluded "An aggressive program could develop an NTP system capable of executing the baseline mission [a crewed mission to Mars duringopposition] in 2039."[24]

In April 2021, DARPA announced the start of DRACO by awarding 18-month Phase 1 contracts toGeneral Atomics for the nuclear reactor concept design ($22 million), and toBlue Origin ($2.5 million) and Lockheed Martin ($2.9 million) for their competing operation system and demonstration system concept designs.[25][26]

In January 2023, NASA and DARPA announced their collaboration on DRACO, dividing the $499 million program between them for Phases 2 and 3.[7][27] NASA is to be responsible for the propulsion system and nuclear reactor, and DARPA is to lead the vehicle and integration requirements, mission concept of operations, nuclear regulatory approvals and launch authority.[7] The U.S. Space Force plans to launch DRACO on either a SpaceX Falcon 9 or aUnited Launch Alliance Vulcan Centaur.[28]

On July 26, 2023, DARPA and NASA announced the awarding of a contract to Lockheed Martin and BWX Advanced Technologies (BWXT) for DRACO Phases 2 and 3 to design, build and demonstrate the experimental NTR for the2027 launch.[27][29] BWXT is slated to design and build the reactor, manufacture the fuel and deliver the complete subsystem for integration into the DRACO vehicle.[30]

Design

[edit]

The main design features of DRACO include the following:[31][32]

  • Thenuclear thermal propulsion (NTP) engine will consist of a fission reactor that transfers heat to a liquid propellant, in this case,liquid hydrogen. That heat will convert the hydrogen into a gas that expands through a nozzle to provide thrust.
  • The nuclear fuel will consist ofenriched uranium, that is,238U (the most commonly-occurring isotope) together with roughly 20% of235U, thefissile isotope. This level of enrichment is somewhat higher than the 3-5% common inlight water power reactors on Earth,[33] but lower than the roughly 90% enrichment characteristic ofweapons-grade material. The choice of 20% enrichment was made in order to alleviate programmatic and regulatory overhead.[citation needed]

According to a 2019 presidential memorandum,[34] approval for the launch of a spacecraft using uranium having enrichment below 20% (a so-called “Tier 2” vehicle) is required only by the head of the sponsoring agency (in this case, the Secretary of Defense) rather than the White House.[35]

  • The propellant will consist of liquid hydrogen (LH2) stored in acryogenic tank. The hydrogen will be heated by the reactor in less than a second from a temperature of about 20K (-420F) to around 2,700 K. For comparison, typical water temperatures of a modernpressurized water reactor are around 600 K.[citation needed]
  • The reactor will be integrated with anexpander cycle rocket engine. In this design, aturbopump directs high-pressure liquid hydrogen down two paths. The first cools the engine’s nozzle and pressure vessel. Liquid hydrogen in the second path first cools the core support assemblies, then drives the turbopump assembly, the exhaust from which is routed back to the reactor pressure vessel where it absorbs energy from the fission reaction. The superheated gas is then expanded out through the nozzle to provide thrust.[citation needed]
  • While details of the design thrust level have not been released, the design goal is said[31] to be aspecific impulse in excess of 800 seconds. (This is the length of time that the rocket can accelerate its own initial mass at a constant 1 gravity.[36]) This would represent an increase of about 350 seconds compared with the specific impulse of theRL10, a liquid-fuel cryogenic rocket engine built in the United States byAerojet Rocketdyne and which is used forCentaur upper stage of theAtlas V.[37]
  • Currently it is uncertain how difficult it might be to maintain the hydrogen propellant in a liquid state for long periods of time, as would be required for trips to Mars.[38] In-space liquid cryogenic propellant transfer has not yet been demonstrated, but Lockheed Martin is developing a refueling vehicle to supportBlue Origin’s Blue Moon lunar lander, and discussions are said to be ongoing about the possibility of installing a refueling port on DRACO.[31]

Development and testing

[edit]

Phase 2 of the DRACO program will involve a test of the NTR engine without nuclear fuel, while Phase 3 will include assembly of the fueled NTR with the stage, environmental testing, and space launch to conduct experiments on the NTR and its reactor.[39] TheU.S. Department of Energy will provideHALEU metal to BWX Technologies for processing into low-enriched fuel.[40] The amount of HALEU utilized for the vehicle has sparked some safety concerns among industry experts and the science community.[41]

In Phase 2, the engine will be evaluated in a cold-flow test with a nonnuclear engine mock-up to assess the mechanical integrity of the core. Such tests were conducted during the Rover/NERVA program in order to study ways to prevent the core from being destroyed from the pressure and high mass flow rates due to the engine’s turbomachinery.[42]

Phase 3 will address launch and space environments testing, assembly integration and testing of the host platform, loads testing, and learning how to interface and command the engine before it is sent to space. During the Phase 3 demonstration, the spacecraft will be launched into a high orbit around Earth, between 435 and 1,240 miles (700 to 2,000 kilometers) above the surface.[31] Once in space, DRACO's reactor is not planned to be activated until it is established in a safe orbit. The minimum orbital altitude is determined by the estimated time it would take for the fission products to decay to the radioactivity level present at launch. In the case of the DRACO reactor, that is about 300 years, which requires an orbit above about 700 km if the orbital decay time is to exceed that value.[31]

According to a timeline in NASA's FY 2025 Budget Estimate document presented to Congress, the project aimed to begin the implementation phase in September 2024.[43] However, that date has passed, and more recently, it was reported[44] that Lockheed Martin Corp. will demonstrate its technology "as early as 2027", but that launch date has since been put on hold by nuclear reactor test requirements.[13]

Program termination

[edit]

DARPA did not include funding for nuclear thermal or electric propulsion programs in its FY2026 budget, whose cuts are being implemented within NASA itself in accordance to the White House goals.[45] DARPA canceled its five-year-old DRACO project, citing a declining return on investment. According to DARPA Deputy Director Rob McHenry, the original rationale for DRACO—high launch costs and the projected efficiency of nuclear thermal engines—has been undermined by significant reductions in launch expenses driven by SpaceX and the potential of Starship. As these launch costs dropped, the benefits of nuclear thermal propulsion no longer justified its high research and development costs.[46]

References

[edit]
  1. ^"DARPA and NASA pick Lockheed Martin to demonstrate DRACO nuclear rocket" Geekwire, July 23, 2023.
  2. ^Erwin, Sandra (31 October 2023)."Space Force assigns 21 national security missions to ULA and SpaceX".SpaceNews. Retrieved22 May 2024.
  3. ^abMike Wall (26 July 2023)."NASA, DARPA to launch nuclear rocket to orbit by early 2026".Space.com. Retrieved13 April 2024.
  4. ^ab"Lockheed Martin Selected to Develop Nuclear-Powered Spacecraft".Media - Lockheed Martin. Retrieved13 April 2024.
  5. ^"NASA has sights set on Mars with help from a nuclear rocket engine".NBC News. 22 May 2023. Retrieved10 May 2024.
  6. ^abFoust, Jeff (26 July 2023)."NASA and DARPA select Lockheed Martin to develop DRACO nuclear propulsion demo".SpaceNews. Retrieved12 May 2024.
  7. ^abc"NASA, DARPA Will Test Nuclear Engine for Future Mars Missions". 24 January 2023. Retrieved22 May 2024.
  8. ^"BWXT to begin work on cislunar nuclear rocket engine and fuel".World Nuclear News. 26 July 2023. Retrieved12 May 2024.
  9. ^"NASA, DARPA Partner with Industry on Mars Rocket Engine".NASA. 26 July 2023. Retrieved13 April 2024.
  10. ^"(Nu)clear the Way: The Future of Nuclear Propulsion is Here".Lockheed Martin. Retrieved13 April 2024.
  11. ^Machi, Vivienne (20 November 2024)."Space Ops: Powering National Security Space With Nuclear".Aviation Week. Retrieved22 November 2024.
  12. ^Chang, Kenneth (26 July 2023)."NASA Seeks a Nuclear-Powered Rocket to Get to Mars in Half the Time".The New York Times.ISSN 0362-4331. Retrieved10 May 2024.
  13. ^abMachi, Vivienne (17 January 2025)."Nuclear Reactor Test Requirements Put DRACO Launch Plans On Hold".Aviation Week & Space Technology. Gregory D. Hamilton. Retrieved4 May 2025.
  14. ^abcClark, Stephen (3 June 2025)."Some parts of Trump's proposed budget for NASA are literally draconian". Ars Technica. Retrieved14 June 2025.
  15. ^Williams, Matthew (2 May 2025)."The White House Releases its 2026 Budget Request for NASA. Cuts to SLS, Gateway and Orion".Universe Today. Retrieved4 May 2025.
  16. ^FY26 Budget Technical Supplement(PDF) (Report). NASA. May 2025. p. ST-8. Retrieved28 June 2025.
  17. ^Hitchens, Theresa (27 June 2025)."DARPA's DRACO nuclear propulsion project ROARs no more".Breaking Defense. Retrieved28 July 2025.
  18. ^Foust, Jeff (2 July 2025)."DARPA says decreasing launch costs, new analysis led it to cancel DRACO nuclear propulsion project". SpaceNews.com. Retrieved7 July 2025.
  19. ^abcWaid, Jack (21 June 2021)."History in Two: Manned Nuclear Aircraft Program".Air Force Materiel Command. Retrieved15 May 2024.
  20. ^abcMcMillan, Tim (4 October 2023)."Air Force research lab takes giant leap into the new space age with plans for nuclear-powered spacecraft systems".thedebrief.org. Retrieved15 May 2024.
  21. ^"Nuclear Pulse Propulsion: Gateway to the Stars".ans.org. Retrieved13 April 2024.
  22. ^abButz Jr., J. S. (1 June 1961)."Rover—the Nuclear Way to Space".airandspaceforces.com. Retrieved14 May 2024.
  23. ^abc"Nuclear Rockets".NASA. Retrieved14 May 2024.
  24. ^abcSpace Nuclear Propulsion for Human Mars Exploration (Report). Washington, DC: The National Academies Press. 2021.doi:10.17226/25977.ISBN 978-0-309-68480-4.
  25. ^Erwin, Sandra (12 April 2021)."DARPA selects Blue Origin, Lockheed Martin to develop spacecraft for nuclear propulsion demo".SpaceNews. Retrieved2 June 2024.
  26. ^"DARPA Selects Performers for Phase 1 of Demonstration Rocket for Agile Cislunar Operations (DRACO) Program".darpa.mil. 12 April 2021. Retrieved3 June 2024.
  27. ^abHitchens, Theresa (26 July 2023)."DARPA, NASA tap Lockheed Martin to design, build DRACO nuclear rocket for deep space missions".Breaking Defense. Archived fromthe original on 16 March 2024. Retrieved9 May 2024.
  28. ^Foust, Jeff (26 July 2023)."NASA and DARPA select Lockheed Martin to develop DRACO nuclear propulsion demo". Space News. Retrieved28 June 2025.
  29. ^Davenport, Christian (27 July 2023)."NASA, Pentagon award contract to build nuclear-powered rocket engine".Washington Post.ISSN 0190-8286. Retrieved10 May 2024.
  30. ^"BWXT to Provide Nuclear Reactor Engine and Fuel for DARPA Space Project".BWXT.com.BWX Technologies, Inc. 26 July 2023. Retrieved10 June 2024.
  31. ^abcdeNorris, Guy (14 August 2023), "Going Nuclear",Aviation Week and Space Technology
  32. ^Krywko, Jacek (22 July 2024)."We're building nuclear spaceships again—this time for real".Ars Technica. Retrieved23 July 2024.
  33. ^Connolly, Thomas J. (1978).Foundations of Nuclear Engineering. New York: John Wiley & Sons. p. 288.ISBN 9780471168584.
  34. ^"Launch of Spacecraft Containing Space Nuclear Systems" (Document). National Security Presidential Memorandum-20. 20 August 2019.
  35. ^Mccallum, Peter (6–9 April 2020).Improvements to the Nuclear Launch Approval Process and Opportunities for New Missions(PDF). Nuclear and Emerging Technologies for Space 2020: Track 3: Mission Concepts and Policy for Nuclear Space Systems. Oak Ridge National Laboratory.
  36. ^Goodger, E. M. (1970).Principles of Spaceflight Propulsion. Elsevier.ISBN 9781483158600.
  37. ^"RL10 Propulsion System"(PDF).l3harris.com. Retrieved28 June 2025.
  38. ^Celnikier, L. M. (1993).Basics of Space Flight. Gif-sur-Yvette, France: Editions Frontieres.ISBN 9782863321317.
  39. ^"Demonstration Rocket for Agile Cislunar Operations (DRACO)".darpa.mil. Retrieved12 May 2024.
  40. ^"DARPA Kicks Off Design, Fabrication for DRACO Experimental NTR Vehicle".darpa.mil. 26 July 2023. Retrieved15 May 2024.
  41. ^Krywko, Jacek (10 June 2024)."DARPA's planned nuclear rocket would use enough fuel to build a bomb".Ars Technica. Retrieved16 June 2024.
  42. ^"Leading DRACO to launch: An interview with DARPA's Tabitha Dodson".ans.org/news/. 28 July 2023. Retrieved28 June 2024.
  43. ^"FY 2025 Budget Estimates"(PDF).
  44. ^"Researchers eye space nuclear thermal propulsion for space maneuver warfare and to cut transit time to Mars".militaryaerospace.com. 18 December 2024. Retrieved1 January 2025.
  45. ^"News | NASA and DARPA Kill DRACO Nuclear Rocket, Shift Focus to".tlpnetwork.com. Retrieved28 July 2025.
  46. ^Hitchens, Theresa (27 June 2025)."DARPA's DRACO nuclear propulsion project ROARs no more".Breaking Defense. Retrieved28 July 2025.

External links

[edit]

Public Domain This article incorporatespublic domain material from websites or documents of theUnited States government.

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