Thermophotovoltaic energy conversion offers a means of efficiently converting heat into electrical power. This has potential benefits for space nuclear reactor power systems currently in development. The primary obstacle to space operation of thermophotovoltaic devices appears to be the low heat rejection temperatures which necessitate large radiator areas. A study of the tradespace between efficiency and radiator size indicates that feasible multi-junction TPV efficiencies result in...
Topics: Nuclear reactors, Electric power, Space nuclear fission reactor, Thermphotovoltaics,...
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292
Jun 21, 2010
06/10
by
NON
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Telemetry simulations, radar equipment and experiments, and related supporting research for Deep Space Network
Topics: NUCLEAR ELECTRIC PROPULSION, SPACECRAFT DESIGN, UNMANNED SPACECRAFT, COMPUTER PROGRAMMING, LAUNCH...
A 2 kW Brayton Power Conversion Unit (PCU) and a xenon ion thruster were integrated with a Power Management and Distribution (PMAD) system as part of a Nuclear Electric Propulsion (NEP) Testbed at NASA's Glenn Research Center. Brayton converters and ion thrusters are potential candidates for use on future high power NEP missions such as the proposed Jupiter Icy Moons Orbiter (JIMO). The use of existing lower power test hardware provided a cost-effective means to investigate the critical...
Topics: NASA Technical Reports Server (NTRS), BRAYTON CYCLE, ION ENGINES, NUCLEAR ELECTRIC PROPULSION,...
The National Aeronautics and Space Administration (NASA) has established a requirement for Nuclear Electric Propulsion (NEP) technology for robotic planetary science mission applications with potential future evolution to systems for piloted Mars vehicles. To advance the readiness of NEP for these challenging missions, a near-term flight demonstration on a meaningful robotic science mission is very desirable. The requirements for both near-term and outer planet science missions are briefly...
Topics: NASA Technical Reports Server (NTRS), MANNED MARS MISSIONS, NUCLEAR ELECTRIC PROPULSION, PROPULSION...
The NASA Glenn Research Center (GRC) is pursuing the development of Brayton cycle power conversion for various NASA initiatives. Brayton cycle power systems offer numerous advantages for space power generation including high efficiency, long life, high maturity, and broad scalability. Candidate mission applications include surface rovers and bases, advanced propulsion vehicles, and earth orbiting satellites. A key advantage is the ability for Brayton converters to span the wide range of power...
Topics: NASA Technical Reports Server (NTRS), BRAYTON CYCLE, NUCLEAR ELECTRIC POWER GENERATION, NUCLEAR...
Nuclear fission has been used as a reliable source for utility power in the United States for decades. Even in the 1940's, long before the United States had a viable space program, the theoretical benefits of nuclear power as applied to space travel were being explored. These benefits include long-life operation and high performance, particularly in the form of vehicle power density, enabling longer-lasting space missions. The configurations for nuclear rocket systems and chemical rocket...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR FISSION, THERMAL ENERGY, ROCKET ENGINES, NUCLEAR...
The performance of Nuclear Electric Propulsion (NEP) in transporting cargo and propellant from Low Earth Orbit (LEO) to the first Earth-Moon Lagrange point (EML1) is examined. The baseline NEP vehicle utilizes a fission reactor system with Brayton power conversion for electric power generation to power multiple liquid hydrogen magnetoplasmadynamic (MPD) thrusters. Vehicle characteristics and performance levels are based on technology availability in a fifteen to twenty year timeframe. Results...
Topics: NASA Technical Reports Server (NTRS), CISLUNAR SPACE, LOW EARTH ORBITS, NUCLEAR ELECTRIC...
This paper describes the concept and preliminary component testing of a gas-cooled, UN-fueled, pin-type reactor which uses He/Xe gas that goes directly into a recuperated Brayton system to produce electricity for nuclear electric propulsion. This Direct-Drive Gas-Cooled Reactor (DDG) is designed to be subcritical under water or wet- sand immersion in case of a launch accident. Because the gas-cooled reactor can directly drive the Brayton turbomachinery, it is possible to configure the system...
Topics: NASA Technical Reports Server (NTRS), GAS COOLED REACTORS, FABRICATION, SYSTEMS ENGINEERING, GAS...
The fundamental capability of Nuclear Thermal Propulsion (NTP) is game changing for space exploration. A first generation Nuclear Cryogenic Propulsion Stage (NCPS) based on NTP could provide high thrust at a specific impulse above 900 s, roughly double that of state of the art chemical engines. Characteristics of fission and NTP indicate that useful first generation systems will provide a foundation for future systems with extremely high performance. The role of the NCPS in the development of...
Topics: NASA Technical Reports Server (NTRS), CRYOGENICS, NUCLEAR PROPULSION, PROPULSION SYSTEM...
No abstract available
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT PROPULSION, ELECTROSTATIC PROPULSION,...
An interagency Nuclear Safety Working Group (NSPWG) was chartered to recommend nuclear safety policy, requirements, and guidelines for the Space Exploration Initiative (SEI) nuclear propulsion program. These recommendations, which are contained in this report, should facilitate the implementation of mission planning and conceptual design studies. The NSPWG has recommended a top-level policy to provide the guiding principles for the development and implementation of the SEI nuclear propulsion...
Topics: NASA Technical Reports Server (NTRS), AEROSPACE SAFETY, MISSION PLANNING, NUCLEAR ELECTRIC...
The topics are presented in viewgraph form and include the following: nuclear propulsion background; schedule for the nuclear electric propulsion (NEP) project; NEP for the Space Exploration Initiative; NEP on-going systems tasks; 20KWe mission/system study; and agenda.
Topics: NASA Technical Reports Server (NTRS), MISSION PLANNING, NUCLEAR ELECTRIC PROPULSION, NUCLEAR...
The Nuclear Electric Propulsion (NEP) system optimization code consists of a master module and various submodules. Each of the submodules represents a subsystem within the total NEP power system. The master module sends commands and input data to each of the submodules and receives output data back. Rocketdyne was responsible for preparing submodules for the power conversion (both K-Rankine and Brayton), heat rejection, and power management and distribution.
Topics: NASA Technical Reports Server (NTRS), COMPUTER PROGRAMS, MISSION PLANNING, NUCLEAR ELECTRIC...
The Jupiter Icy Moons Orbiter (JIMO) is a bold new mission being developed by NASA's Office of Space Science under Project Prometheus. JIMO is examining the potential of nuclear electric propulsion (NEP) technology to efficiently deliver scientific payloads to three of Jupiter's moons: Callisto, Ganymede, and Europa. A critical element of the NEP spacecraft is the space reactor power system (SRPS), consisting of the nuclear reactor, power conversion, heat rejection, and power management and...
Topics: NASA Technical Reports Server (NTRS), GANYMEDE, ICE, JUPITER (PLANET), SOLAR CELLS, SOLAR...
Nuclear electric propulsion has been identified as an enabling technology for future NASA space science missions, such as the Jupiter Icy Moons Orbiter (JIMO) now under study. An important element of the nuclear electric propulsion spacecraft is the power conversion system, which converts the reactor heat to electrical power for use by the ion propulsion system and other spacecraft loads. The electrical integration of the power converter and ion thruster represents a key technical challenge in...
Topics: NASA Technical Reports Server (NTRS), BRAYTON CYCLE, ION ENGINES, POWER CONVERTERS, ION PROPULSION,...
Evolutionary computational (EC) techniques such as genetic algorithms (GA) have been identified as promising methods to explore the design space of mechanical and electrical systems at the earliest stages of design. In this paper the authors summarize their research in the use of evolutionary computation to develop preliminary designs for various space systems. An evolutionary computational solver developed over the course of the research, X-TOOLSS (Exploration Toolset for the Optimization of...
Topics: NASA Technical Reports Server (NTRS), GENETIC ALGORITHMS, AEROSPACE SYSTEMS, COMPLEX SYSTEMS,...
NASA has initiated a technology program to establish the readiness of nuclear propulsion technology for the Space Exploration Initiative (SEI). This program was initiated with a very modest effort identified with nuclear thermal propulsion (NTP); however, nuclear electric propulsion (NEP) is also an integral part of this program and builds upon NASA's Base Research and Technology Program in power and electric propulsion as well as the SP-100 space nuclear power program. Although the Synthesis...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC PROPULSION, ROBOTICS, SPACE EXPLORATION,...
The objective of this study was to establish the initial quantitative reliability bounds for nuclear electric propulsion systems in a manned Mars mission required to ensure crew safety and mission success. Finding the reliability bounds involves balancing top-down (mission driven) requirements and bottom-up (technology driven) capabilities. In seeking this balance we hope to accomplish the following: (1) provide design insights into the achievability of the baseline design in terms of...
Topics: NASA Technical Reports Server (NTRS), MISSION PLANNING, NUCLEAR ELECTRIC PROPULSION, RELIABILITY,...
This report serves as the second Addendum to NASA-SP-2009-566, "Human Exploration of Mars Design Reference Architecture 5.0." The data and descriptions contained within this Addendum capture some of the key assessments and studies produced since publication of the original document, predominately covering those conducted from 2009 through 2012. The assessments and studies described herein are for the most part independent stand-alone contributions. Effort has not been made to...
Topics: NASA Technical Reports Server (NTRS), MARS SURFACE, NUCLEAR ELECTRIC PROPULSION, SPACECRAFT...
Under the NASA Exploration Technology Development Program, and in partnership with the Department of Energy (DOE), NASA is conducting a project to mature Fission Power System (FPS) technology. A primary project goal is to develop viable system options to support future NASA mission needs for nuclear power. The main FPS project objectives are as follows: 1) Develop FPS concepts that meet expected NASA mission power requirements at reasonable cost with added benefits over other options. 2)...
Topics: NASA Technical Reports Server (NTRS), NASA PROGRAMS, TECHNOLOGY UTILIZATION, AEROSPACE VEHICLES,...
NASA has completed a preliminary mission and systems study of nuclear electric propulsion (NEP) systems for 'split-sprint' human exploration and related robotic cargo missions to Mars. This paper describes the study, the mission architecture selected, the NEP system and technology development needs, proposed development schedules, and estimated development costs. Since current administration policy makers have delayed funding for key technology development activities that could make Mars...
Topics: NASA Technical Reports Server (NTRS), MANNED MARS MISSIONS, NUCLEAR ELECTRIC PROPULSION, PROPULSION...
This paper describes potential heat rejection design concepts for Brayton power conversion systems. Brayton conversion systems are currently under study by NASA for Nuclear Electric Propulsion (NEP) and surface power applications. The Brayton Heat Rejection Subsystem (HRS) must dissipate waste heat generated by the power conversion system due to inefficiencies in the thermal-to-electric conversion process. Sodium potassium (NaK) and H2O are two coolant working fluids that have been investigated...
Topics: NASA Technical Reports Server (NTRS), BRAYTON CYCLE, HEAT PIPES, NUCLEAR ELECTRIC PROPULSION,...
Radiator technology is discussed in the context of the Civilian Space Technology Initiative's (CSTI's) high capacity power-thermal management project. The CSTI project is a subset of a project to develop a piloted Mars nuclear electric propulsion (NEP) vehicle. The following topics are presented in vugraph form: advanced radiator concepts; heat pipe codes and testing; composite materials; radiator design and integration; and surface morphology.
Topics: NASA Technical Reports Server (NTRS), AEROSPACE ENGINEERING, DESIGN ANALYSIS, HEAT PIPES, MANNED...
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May 31, 2011
05/11
by
Martin, Lynne; Orasanu, Judith; Villeda, Eri
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One way to enhance the effectiveness of Special Purpose Operational Training' (SPOT) debriefing sessions may be for instructors to make explicit connections between the Crew Resource Management (CRM) concepts a carrier advocates and the behaviors displayed by the crew in question. A tool listing key behaviors from the scenario was devised, accompanied by an instructors' training session in which links were made between the behaviors and the underlying CRM processes they reflect. The aim of the...
Topics: NUCLEAR ELECTRIC PROPULSION, MOLTEN SALTS, REACTOR TECHNOLOGY, PLANETARY SURFACES, LIQUID METALS
Current designs for out of core thermionic energy conversion (TEC) to power nuclear electric propulsion (NEP) were evaluated. Approaches to improve out of core TEC are emphasized and probabilities for success are indicated. TEC gains are available with higher emitter temperatures and greater power densities. Good potentialities for accommodating external high temperature, high power density TEC with heat pipe cooled reactors exist.
Topics: NASA Technical Reports Server (NTRS), ENERGY CONVERSION EFFICIENCY, NUCLEAR ELECTRIC PROPULSION,...
A discussion of Nuclear Electric Propulsion (NEP) thrusters and facilities is presented in vugraph form. The NEP thrusters are discussed in the context of the following three items: (1) establishing a 100 H test capability for 100-kW magnetoplasmadynamic (MPD) thrusters; (2) demonstrating a lightweight 20-kW krypton ion thruster; and (3) the optimization of the design of low-mass power processor transformers. The primary accomplishment at NEP facilities was the completion of the Electric...
Topics: NASA Technical Reports Server (NTRS), ELECTRIC ROCKET ENGINES, ION PROPULSION,...
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Jun 21, 2010
06/10
by
NON
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Shock tests on Mariner Venus 67 prototype data automation subsystems to evaluate multilayer laminate packaging
Topics: CATHODES, NUCLEAR ELECTRIC PROPULSION, GLOW DISCHARGES, ION ENGINES, MAGNETOHYDRODYNAMIC...
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May 22, 2011
05/11
by
NON
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The present invention provides a fixture for supporting an elongated specimen for crush testing. The fixture comprises a base plate, four guiding rods, a sliding plate, four support rods and two collars. The guiding rods connect to the base plate and extend in a direction substantially perpendicular to the base plate. The sliding plate has linear bearings which encircle the guiding rods and enable translation of the sliding plate along the axis of each guiding rod. The four supporting rods...
Topics: NUCLEAR ELECTRIC PROPULSION, PROTONS, SPACECRAFT DESIGN, SPACECREWS, NUCLEAR ROCKET ENGINES,...
No abstract available
Topics: NASA Technical Reports Server (NTRS), NUCLEAR FISSION, NUCLEAR ELECTRIC PROPULSION, NUCLEAR ROCKET...
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359
Jul 26, 2010
07/10
by
Moynihan, C. T.; Shahriari, M. R.; Bardakci, T
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No Abstract Available
Topics: NUCLEAR ELECTRIC PROPULSION, URANIUM, NUCLEAR REACTORS, OUTER PLANETS EXPLORERS, SPACECRAFT...
The following topics are addressed: (1) in-space propulsion impacts; (2) electric propulsion; (3) mission impacts of electric propulsion; and (4) summaries of electric propulsion status and solar and nuclear propulsion.
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC PROPULSION, SOLAR ELECTRIC PROPULSION,...
A modular, multi-reactor power system and vehicle configuration for piloted nuclear electric propulsion (NEP) missions to Mars is presented. Such a design could provide enhanced system and mission reliability, allowing a comfortable safety margin for early manned flights, and would allow a range of piloted and cargo missions to be performed with a single power system design. Early use of common power modules for cargo missions would also provide progressive flight experience and validation of...
Topics: NASA Technical Reports Server (NTRS), MANNED MARS MISSIONS, MODULARITY, NUCLEAR ELECTRIC POWER...
Two recently developed FORTRAN computer codes for high power Brayton and Rankine thermodynamic cycle analysis for space power applications are presented. The codes were written in support of an effort to develop a series of subsystem models for multimegawatt Nuclear Electric Propulsion, but their use is not limited just to nuclear heat sources or to electric propulsion. Code development background, a description of the codes, some sample input/output from one of the codes, and state future...
Topics: NASA Technical Reports Server (NTRS), BRAYTON CYCLE, COMPUTER PROGRAMS, NUCLEAR ELECTRIC...
Economical unmanned earth orbit transportation for large payloads is evaluated. The high exhaust velocity achievable with electric propulsion is attractive because it minimizes the propellant that must be carried to low earth orbit. Propellant transport is a principal cost item. Electric propulsion subsystems utilizing advanced ion thrusters are compared to magnetoplasmadynamic (MPD) thrust subsystems. For very large payloads, a large lift vehicle is needed to low earth orbit, and argon...
Topics: NASA Technical Reports Server (NTRS), EARTH ORBITS, NUCLEAR ELECTRIC PROPULSION, SOLAR ELECTRIC...
Space nuclear power systems are considered for use in those particular spacecraft applications for which nuclear power systems offer unique advantages over solar and/or chemical space power systems. Both isotopic and reactor heated space electrical power units are described in an attempt to illustrate their operating characteristics, spacecraft integration aspects, and factory-to-end of mission operational considerations. The status of technology developments in nuclear power systems is...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC POWER GENERATION, NUCLEAR ELECTRIC...
The effects of trip time, propulsion time, and specific powerplant mass are studied for optimized unmanned probe spacecraft on missions to Uranus with nuclear-electric propulsion systems. Electric propulsion is confined to a single thrust period at the beginning of each mission. Mission profiles include both high-thrust and electric-propulsion Earth-departure modes for planet flyby and orbital capture. Effects of propulsion time and propulsion system parameters are evaluated, and typical design...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC PROPULSION, THRUST PROGRAMMING, UNMANNED...
The development of electric propulsion systems is discussed and the benefits of these systems to various space mission requirements are outlined. The characteristics and development status of 8 and 30 cm mercury ion thrusters and solar electric propulsion systems are reported. In addition the advantages of an inert gas thruster for Earth orbital missions are examined and include its capability for operation at higher values of specific impulse, the ease at which it can be integrated with space...
Topics: NASA Technical Reports Server (NTRS), ELECTRIC PROPULSION, LARGE SPACE STRUCTURES, SPACECRAFT...
The documentation of the Trajectory Generation and System Characterization Model for the Cislunar Low-Thrust Spacecraft is presented in Technical and User's Manuals. The system characteristics and trajectories of low thrust nuclear electric propulsion spacecraft can be generated through the use of multiple system technology models coupled with a high fidelity trajectory generation routine. The Earth to Moon trajectories utilize near Earth orbital plane alignment, midcourse control dependent...
Topics: NASA Technical Reports Server (NTRS), ALGORITHMS, CISLUNAR SPACE, LOW THRUST, MIDCOURSE...
The Space Exploration Initiative is considering the use of low thrust (nuclear electric, solar electric) and intermediate thrust (nuclear thermal) propulsion systems for transfer to Mars and back. Due to the duration of such a mission, a low thrust minimum-fuel solution is of interest; a savings of fuel can be substantial if the propulsion system is allowed to be turned off and back on. This switching of the propulsion system helps distinguish the minimal-fuel problem from the well-known...
Topics: NASA Technical Reports Server (NTRS), ALGORITHMS, FUEL CONSUMPTION, LOW THRUST PROPULSION, NUCLEAR...
The objective of the Nuclear Electric Propulsion (NEP) space test program is to launch an NEP satellite powered by the Russion Topaz 2 reactor by Dec. 1995. The primary goals of the NEP space test program are as follows: (1) demonstrate the feasibility of launching a space nuclear power system; (2) demonstrate and orbit adjust capability using NEP; (3) evaluate the in-orbit performance of the Topaz 2 reactor and selected electric thrusters; and (4) measure, analyze, and model the NEP...
Topics: NASA Technical Reports Server (NTRS), ARTIFICIAL SATELLITES, NUCLEAR ELECTRIC PROPULSION, SPACE...
The exploration of our solar system will require spacecraft with much greater capability than spacecraft which have been launched in the past. This is particularly true for exploration of the outer planets. Outer planet exploration requires shorter trip times, increased payload mass, and ability to orbit or land on outer planets. Increased capability requires better propulsion systems, including increased specific impulse. Chemical propulsion systems are not capable of delivering the...
Topics: NASA Technical Reports Server (NTRS), SPACE MISSIONS, PROPULSION SYSTEM PERFORMANCE, PROPULSION...
No abstract available
Topics: NASA Technical Reports Server (NTRS), PROPULSION SYSTEM CONFIGURATIONS, SPACECRAFT RADIATORS,...
A crewed mission to Mars poses a signi cant challenge in dealing with the physiolog- ical issues that arise with the crew being exposed to a near zero-gravity environment as well as signi cant solar and galactic radiation for such a long duration. While long sur- face stay missions exceeding 500 days are the ultimate goal for human Mars exploration, short round trip, short surface stay missions could be an important intermediate step that would allow NASA to demonstrate technology as well as...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC PROPULSION, LOW THRUST PROPULSION, SOLAR...
Nuclear electric propulsion (NEP) vehicles will be needed for future manned missions to Mars and beyond. Candidate designs must be identified for further detailed design from a large array of possibilities. Genetic algorithms have proven their utility in conceptual design studies by effectively searching a large design space to pinpoint unique optimal designs. This research combined analysis codes for NEP subsystems with a genetic algorithm. The use of penalty functions with scaling ratios was...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR ELECTRIC PROPULSION, MANNED SPACE FLIGHT, SPACECRAFT...
The fundamental capability of Nuclear Thermal Propulsion (NTP) is game changing for space exploration. A first generation Nuclear Cryogenic Propulsion Stage (NCPS) based on NTP could provide high thrust at a specific impulse above 900 s, roughly double that of state of the art chemical engines. The foundation provided by development and utilization of a NCPS could enable development of extremely high performance systems. The role of the NCPS in the development of advanced nuclear propulsion...
Topics: NASA Technical Reports Server (NTRS), NUCLEAR PROPULSION, PROPULSION SYSTEM CONFIGURATIONS,...
NASA is developing technologies for nuclear electric propulsion for proposed deep space missions in support of the Exploration initiative under Project Prometheus. Electrical power produced by the combination of a fission-based power source and a Brayton power conversion and distribution system is used by a high specific impulse ion propulsion system to propel the spaceship. The ion propulsion system include the thruster, power processor and propellant feed system. A power processor technology...
Topics: NASA Technical Reports Server (NTRS), DEEP SPACE, NUCLEAR ELECTRIC PROPULSION, SPACE MISSIONS,...
A theoretical investigation was conducted to estimate the spectral properties of argon as a function of pressure, temperature, and wave number. The spectral characteristics of the argon buffer gas exert a strong influence on radiative energy transfer in the in-reactor test configuration of the nuclear light bulb engine. An existing computer program was modified and used to calculate the spectral absorption coefficients of argon at total pressures of 50, 100, 250, 500, 750 and 1000 atm in the...
Topics: NASA Technical Reports Server (NTRS), ABSORPTION SPECTRA, ALUMINUM, ARGON, SILICON, SPECTRAL...
Alkali metal boilers are of interest for application to future space Rankine cycle power conversion systems. Significant progress on such boilers was accomplished in the 1960's and early 1970's, but development was not continued to operational systems since NASA's plans for future space missions were drastically curtailed in the early 1970's. In particular, piloted Mars missions were indefinitely deferred. With the announcement of the Space Exploration Initiative (SEI) in July 1989 by President...
Topics: NASA Technical Reports Server (NTRS), ALKALI METALS, BOILERS, INTERPLANETARY SPACE, MANNED MARS...
The application of a nuclear electric propulsion (NEP) stage in the exploration of near-earth, cometary, and planetary space was discussed. The NEP stage is powered by a liquid-metal-cooled, fast spectrum thermionic reactor capable of providing 120 kWe for 20,000 hours. This power is used to drive a number of mercury ion bombardment thrusters with specific impulse in the range of 4000-5000 seconds. The NEP description, characteristics, and functional requirements are discussed. These...
Topics: NASA Technical Reports Server (NTRS), COMETS, NUCLEAR ELECTRIC PROPULSION, SPACE EXPLORATION, ION...
The objective of this mission study was to compare laser propulsion to chemical LOX/H2 and nuclear electric propulsion for the specific mission of delivering a 144-metric ton lunar base from low-Earth-orbit to low-lunar-orbit. The basis of comparison was total mass in low-Earth-orbit needed to accomplish this mission. The Office of Exploration approach to establishing the lunar base was to use two vehicles: a nuclear electric propulsion (NEP) vehicle to deliver cargo and a chemical vehicle to...
Topics: NASA Technical Reports Server (NTRS), CHEMICAL PROPULSION, COMPARISON, EARTH ORBITS, LASER POWER...
