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Theodore N. Edelbaum
Observed names:
Edelbaum, T. N.,
Edelbaum, Theodore N.,
T. EDELBAUM,
T. N. EDELBAUM,
T. N. Edelbaum,
T.N. EDELBAUM,
T.N. Edelbaum,
THEODORE EDELBAUM,
THEODORE N. EDELBAUM
show all 9
Observed institutions:
Draper Laboratory,
Analytical Mechanics Associates (United States),
United Technologies (United States),
Massachusetts Institute of Technology
OpenAlex ID:
A5025170153
Propulsion Requirements for Controllable Satellites
1961
·
THEODORE N. EDELBAUM
·
ARS journal
·
338
Optimum low-thrust rendezvous and station keeping
1964
·
THEODORE N. EDELBAUM
·
AIAA Journal
·
92
Optimum power-limited orbit transfer in strong gravity fields
1965
·
THEODORE N. EDELBAUM
·
AIAA Journal
·
75
Energy climbs, energy turns, and asymptotic expansions
1970
·
HENRY J. KELLEY
, THEODORE N. EDELBAUM
·
Journal of Aircraft
·
74
Theory of Maxima and Minima
1962
·
Theodore N. Edelbaum
·
Mathematics in Science and Engineering/Mathematics in science and engineering
·
74
Optimum power-limited orbit transfer in strong gravity fields
1964
·
T. EDELBAUM
·
67
Optimal low thrust geocentric transfer
1973
·
T. EDELBAUM
, L. SACKETT
, et al.
·
AIAA Electric Propulsion Conference
·
55
How many impulses
1967
·
T. N. Edelbaum
·
NASA Technical Reports Server (NASA)
·
53
Fuel optimal reorientation of axisymmetric spacecraft
1970
·
M. V. DIXON
, T. N. EDELBAUM
, et al.
·
Journal of Spacecraft and Rockets
·
43
Minimum Impulse Three-Body Trajectories
1974
·
LOUIS A. D'AMARIO
, THEODORE N. EDELBAUM
·
AIAA Journal
·
42
Minimum Impulse Transfers in the Near Vicinity of a Circular Orbit
1967
·
T. N. Edelbaum
·
The Journal of the Astronautical Sciences
·
40
Optimal Space Trajectories
1969
·
Theodore N. Edelbaum
·
Defense Technical Information Center (DTIC)
·
29
Optimum Low-Thrust Rendezvous and Station Keeping
2003
·
THEODORE N. EDELBAUM
·
Journal of Spacecraft and Rockets
·
26
Optimal Nonplanar Escape from Circular Orbits
1971
·
T. N. EDELBAUM
·
AIAA Journal
·
25
An asymptotic solution for optimum power limited orbit transfer.
1966
·
T. N. EDELBAUM
·
AIAA Journal
·
21
Four-Body Trajectory Optimization
1975
·
C. L. PU
, T. N. EDELBAUM
·
AIAA Journal
·
17
Optimal solar sail spiral to escape
1977
·
L. L. Sackett
, T. N. Edelbaum
·
NASA Technical Reports Server (NASA)
·
16
Applications of snap-50 class powerplants to selected unmanned electric propulsion missions
1965
·
W. R. FlMPLE
, T. N. EDELBAUM
·
Journal of Spacecraft and Rockets
·
14
Fifth and sixth integrals for optimum rocket trajectories in a central field
1970
·
T. N. EDELBAUM
, S. PINES
·
AIAA Journal
·
13
Application of a Finite-Difference Newton-Raphson Algorithm to Problems of Low-Thrust Trajectory Optimization
1966
·
C.P. Van Dine
, W.R. Fimple
, et al.
·
Progress in astronautics and aeronautics
·
13
Optimum Maneuvers for Launching Satellites Into Circular Orbits of Arbitrary Radius and Inclination
1961
·
J. P. CARSTENS
, T. N. EDELBAUM
·
ARS journal
·
13
Minimum impulse three-body trajectories
1973
·
L. D'AMARIO
, T. EDELBAUM
·
11th Aerospace Sciences Meeting
·
12
Optimum thrust-limited orbit transfer in strong gravity fields
1970
·
T. N. Edelbaum
·
Lecture notes in mathematics
·
11
How many impulses/ques/
1966
·
T. EDELBAUM
·
3rd and 4th Aerospace Sciences Meeting
·
11
Minimum-impulse time-free transfer between elliptic orbits
1966
·
T. N. Edelbaum
, F. W. Gobetz
, et al.
·
NASA Technical Reports Server (NASA)
·
7
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Works count:
61
Citation count:
1,233
H-index:
16
I10-index:
24
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