Citation: Ca. Kluever et Sr. Oleson, DIRECT APPROACH FOR COMPUTING NEAR-OPTIMAL LOW-THRUST EARTH-ORBIT TRANSFERS, Journal of spacecraft and rockets, 35(4), 1998, pp. 509-515
Citation: Ca. Kluever et M. Abusaymeh, MERCURY MISSION DESIGN USING SOLAR ELECTRIC PROPULSION SPACECRAFT, Journal of spacecraft and rockets, 35(3), 1998, pp. 411-413
Citation: Ca. Kluever et Bl. Pierson, OPTIMAL EARTH-MOON TRAJECTORIES USING NUCLEAR ELECTRIC PROPULSION, Journal of guidance, control, and dynamics, 20(2), 1997, pp. 239-245
Citation: Ca. Kluever, OPTIMAL EARTH-MOON TRAJECTORIES USING COMBINED CHEMICAL-ELECTRIC PROPULSION, Journal of guidance, control, and dynamics, 20(2), 1997, pp. 253-258
Citation: Ca. Kluever, MAXIMUM-PAYLOAD TRANSFERS TO GEOSYNCHRONOUS ORBIT USING ARCJET THRUSTERS, Journal of spacecraft and rockets, 34(3), 1997, pp. 405-407
Citation: Ca. Kluever, OPTIMAL LOW-THRUST INTERPLANETARY TRAJECTORIES BY DIRECT METHOD TECHNIQUES, The Journal of the astronautical sciences, 45(3), 1997, pp. 247-262
Citation: Ca. Kluever et Kr. Chang, ELECTRIC-PROPULSION SPACECRAFT OPTIMIZATION FOR LUNAR MISSIONS, Journal of spacecraft and rockets, 33(2), 1996, pp. 235-239
Citation: Ca. Kluever et Bl. Pierson, OPTIMAL LOW-THRUST 3-DIMENSIONAL EARTH-MOON TRAJECTORIES, Journal of guidance, control, and dynamics, 18(4), 1995, pp. 830-837
Citation: Ca. Kluever, LOW-THRUST ORBIT TRANSFER GUIDANCE USING AN INVERSE DYNAMICS APPROACH, Journal of guidance, control, and dynamics, 18(1), 1995, pp. 187-189
Citation: Ca. Kluever et Bl. Pierson, VEHICLE-AND-TRAJECTORY OPTIMIZATION OF NUCLEAR ELECTRIC SPACECRAFT FOR LUNAR MISSIONS, Journal of spacecraft and rockets, 32(1), 1995, pp. 126-132
Citation: Bl. Pierson et Ca. Kluever, 3-STAGE APPROACH TO OPTIMAL LOW-THRUST EARTH-MOON TRAJECTORIES, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1275-1282
Citation: Ca. Kluever et Bl. Pierson, OPTIMAL LOW-THRUST EARTH-MOON TRANSFERS WITH A SWITCHING FUNCTION-STRUCTURE, The Journal of the astronautical sciences, 42(3), 1994, pp. 269-283