Pilotiruemaya ekspeditsiya na Mars (Manned Expedition to Mars), Koroteev, A.S., Ed., Moscow: Rossiiskaya akademiya kosmonavtiki im. K.E. Tsiolkovskogo, 2006.
Gorshkov, O., Akimov, V., Koroteev, A., and Semenov, V., A concept of manned mission to Mars. Comparative analysis of variants, in The 60th International Astronautical Congress, Daejon, Korea, 2009, IAC-09-A5.1.9.
Konstantinov, M. and Petukhov, V., The analysis of required characteristics of electric power plant and electric propulsion at realization of one mission of manned expedition onto Mars, in Space Propulsion Conference, San Sebastian, Spain, 2010, 1841662.
Konstantinov, M.S. and Petukhov, V.G., The analysis of one concept of manned mission to Mars, in The 61st International Astronautical Congress, Prague, Czech Republic, 2010, IAC-10-A5.4.6.
Konstantinov, M.S., Loeb, H.W., Petukhov, V.G., and Popov, G.A., One variant of manned mission to Mars with a nuclear electric propulsion, Int. J. Space Technol. Manage. Innovation, 2011, vol. 1, no. 2, pp. 1–17.
Konstantinov, M.S., Loeb, H.W., Petukhov, V.G., and Popov, G.A., Design–ballistic analysis of a manned mission to Mars with a nuclear electric propulsion system, Tr. Mosk. Aviats. Inst., 2011, no. 42.
Konstantinov, M.S. and Petukhov, V.G., The analysis of manned Mars mission with duration of 1000 days, Acta Astronaut., 2012, vol. 73, pp. 122–136.
Klimov, S.S., Joint optimization of trajectory and power-plant parameters of Martian expedition systems with electric propulsion systems, Kosmonavt. Raketostr., 2017, no. 4, pp. 71–84.
Loeb, H.W. and Xiaodong, D., Large-scale radio-frequency ion thrusters for manned Mars missions, in 43rd Congress of the International Astronautical Federation, Washington, D.C., August 28–September 5,
Lebedev, V.N., Raschet dvizheniya kosmicheskogo apparata s maloi tyagoi (Computation of the Motion of a Low-Thrust Spacecraft), Moscow: VTs AN SSSR, 1968.
Grodzovskii, G.L., Ivanov, Yu.N., and Tokarev, V.V., Mekhanika kosmicheskogo poleta. Problemy optimizatsii (Mechanics of Space Flight. Problems of Optimization), Moscow: Nauka, 1975.
Konstantinov, M.S. and Thein, M., Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits, Cosmic Res., 2017, vol. 55, no. 3, pp. 214–223.
Konstantinov, M.S., Orlov, A.A., and Thein M., Analysis of the impact power of the solar power installation on the flight characteristics of the spacecraft with solar electric propulsion to Jupiter, Izv. Ross. Akad. Nauk: Energ., 2017, no. 3, pp. 97–113.
Konstantinov, M.S., Petukhov, V.G., and Thein, M., Analysis for the impact of power of the solar power plant on the characteristics of the project “Interhelio-Probe” at using electric propulsion, Izv. Ross. Akad. Nauk: Energ., 2016, no. 2, pp. 102–117.
Konstantinov, M.S. and Thein, M., Method of interplanetary trajectory optimization for the spacecraft with low thrust and swing-bys, Acta Astronaut., 2017, vol. 136, pp. 297–311.
Pontryagin, L.S., Boltyanskii, V.G., Gamkrelidze, R.V., and Mishchenko, E.F., Matematicheskaya teoriya optimal’nykh protsessov (Mathematical Theory of Optimal Processes), Moscow: Fizmatlit, 1961.
Petukhov, V.G., Homotopic approach to low-thrust trajectory optimization: Numerical technique and tools, in 4th International Conference on Astrodynamics Tools and Techniques, 3–6 May
2010, ESA/ESAC, Madrid, Spain, ESA Proceedings, WPP-308.
Konstantinov, M.S., Petukhov, V.G., and Thein, M., Optimizatsiya traektorii geliotsentricheskikh pereletov (Heliocentric Flight Trajectory Optimization), Moscow: MAI, 2015.