A Grand Tour of the outer planets
Outer planet explorers design for Grand Tour mission, discussing launch parameters, flight paths, environmental hazards, communications, ground control, navigation and power generation
Long, J. E.↗
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The effects of radiation on science instruments during Grand Tour type missions
Radiation effects on components of science instruments used on outer planets Grand Tour mission
Barengoltz, J. B.↗
Satellite encounter opportunities of the Grand Tour missions
Multiple outer planets flyby opportunities during 1976-1980 Grand Tour missions launch period, presenting computer generated specific encounter dates and flyby distances
Penzo, P. A.↗
Asteroid encounters on Grand Tour and other missions which traverse the region beyond Mars
Asteroids flyby approaches during Jupiter missions and Grand Tours, obtaining gravitational deflection of spacecraft trajectories and mass cost estimates
Bender, D. F.↗
An analysis of approach navigation accuracy and guidance requirements for the grand tour mission to the outer planets
The navigation and guidance process for the Jupiter, Saturn and Uranus planetary encounter phases of the 1977 Grand Tour interior mission was simulated. Reference approach navigation accuracies were defined and the relative information content of the various observation types were evaluated. Reference encounter guidance requirements were defined, sensitivities to assumed simulation model parameters were determined and the adequacy of the linear estimation theory was assessed. A linear sequential estimator was used to provide an estimate of the augmented state vector, consisting of the six state variables of position and velocity plus the three components of a planet position bias. The guidance process was simulated using a nonspherical model of the execution errors. Computation algorithms which simulate the navigation and guidance process were derived from theory and implemented into two research-oriented computer programs, written in FORTRAN.
Jones, D. W.↗
Radiation effects on science instruments in Grand Tour type missions
The extent of the radiation effects problem is delineated, along with the status of protective designs for 15 representative science instruments. Designs for protecting science instruments from radiation damage is discussed for the various instruments to be employed in the Grand Tour type missions. A literature search effort was undertaken to collect science instrument components damage/interference effects data on the various sensitive components such as Si detectors, vidicon tubes, etc. A small experimental effort is underway to provide verification of the radiation effects predictions.
Parker, R. H.↗
The effects of radiation on the outer planets grand tour
A handbook is presented which was designed to accompany an oral presentation on the effects of radiation on the outer planets grand tour (OPGT). A summary of OPGT radiation environments expected from natural sources and the radioisotope thermoelectric generators and basic radiation effects and processes are reviewed, and ionization and displacement effects are examined. The presentation summarizes the effects of radiation on miscellaneous spacecraft materials and devices. The annealing and hardening of electronics are described. Special emphasis is placed on microcircuits. Mathematical modeling of circuits affected by radiation and radiation environmental testing are discussed. A review of means of evaluating the performance and correcting failures of irradiated devices is also presented.
Source record↗
Magnetometer instrument team studies for the definition phase of the outer planets grand tour
The objectives of magnetic field investigations on missions to the outer planets were defined as well as an instrumentation system, a program of studies and instrument development tasks was proposed for the mission definition phase of the Outer Planets Grand Tour project. A report on the status of this program is given. Requirements were also established for the spacecraft and the mission which would insure their compatibility with the magnetic field investigation proposed for the outer planets missions and developed figures of merit for encounter trajectories. The spacecraft-instrumentation interface and the on-board data handling system were defined in various reports by the Project Team and in the reports by the Science Steering Group. The defining program for exploring the outer planets within the more restrictive constraints of the Mariner Jupiter-Saturn project included defining a limited magnetic field investigation.
Coleman, P. J., Jr.↗
Estimating trajectory correction requirements for the Outer Planets Grand Tour missions.
The estimation of trajectory correction requirements for the Outer Planets Grand Tour (OPGT) missions poses a unique and many-faceted problem for the systems analyst. In this paper the navigation concept for the OPGT is developed and illustrated. The limiting accuracies and performance of the combined radio/onboard optical system are examined. The combined orbit determination system is characterized by its accuracy and by its system risks. Such considerations are included with the statistical combination of maneuver estimates to produce preliminary delta V estimates for the planned OPGT missions.
Friedman, L. D.↗
Magnetometer instrument team studies for the definition phase of the outer planets grand tour
The work performed by the magnetic fields investigation team during the mission definition phases of the Outer Planets Grand Tour (OPGT) and the Mariner Jupiter Saturn (MJS) Missions is reported. This work involved three tasks: (1) defining the objectives of the magnetic fields investigations, (2) defining the magnetometer systems required to meet these objectives, and (3) developing and testing hardware elements in certain mission-specific areas.
Coleman, P. J., Jr.↗
Grand Tour outer planet missions definition phase. Part 1: Quantitative imaging of the outer planets and their satellites
A recommended imaging system is outlined for use aboard the Outer Planet Grand Tour Explorer. The system features the high angular resolution capacity necessary to accommodate large encounter distances, and to satisfy the demand for a reasonable amount of time coverage. Specifications for all components within the system are provided in detail.
Belton, M. J. S.↗
Grand Tour outer planet missions definition phase. Part 2: Minutes of meetings and official correspondence
A variety of imaging systems proposed for use aboard the Outer Planet Grand Tour Explorer are discussed and evaluated in terms of optimal resolution capability and efficient time utilization. It is pointed out that the planetary and satellite alignments at the time of encounter dictate a high degree of adaptability and versatility in order to provide sufficient image enhancement over earth-based techniques. Data compression methods are also evaluated according to the same criteria.
Belton, M. J. S.↗
Outer planets grand tours: Planetary radio astronomy team report
Requirements related to scientific observations of planetary radio emissions during outer planets grand tours are discussed. Observations at low frequencies where non-thermal cooperative plasma phenomena play a major role are considered for determining dynamical processes and magnetic fields near a planet. Magnetic field measurements by spacecraft magnetometers, and by radio receivers in their harmonic modes are proposed for interpretation of planetary radio emission.
Warwick, J. W.↗
Grand Tour missions to the outer solar system with Saturn /Intermediate 20/.
Discussion of the hazards, spacecraft features, time schedules, scientific objectives, and experiment packages which would probably characterize Grand Tour missions to the outer planets. The capabilities of the Saturn Intermediate 20 vehicle and supporting subsystems presently envisioned for such missions are outlined on the basis of comparison with other candidate launch vehicles. Hazard estimates are given for asteroid encounters, on-board and external radiation sources, trajectory perturbations, and operational reliability of equipment. Direct, swingby, and multiplanet missions are discussed in terms of launch opportunities, injection velocities, and flight durations. Measurements which should be carried out are evaluated for relevant contributions to knowledge of the outer planets.
Hale, D. P.↗
Orbit determination for a Jupiter orbiter tour of the Galilean satellites
Current NASA planning envisions an ambitious Jupiter tour mission which will arrive at the planet in the year, 1984. The objectives of this mission are to broaden our knowledge of the outer solar system and in particular to extend our understanding of the physical processes at work in the Jupiter and Galilean satellite environment. To achieve these goals, precise spacecraft navigation is a fundamental requirement inasmuch as very near encounters with the satellites are necessary both for the planned scientific investigations and to reduce fuel requirements necessary for orbital insertion about the planet. This paper, deals with problems of producing precise spacecraft state estimates relative to the Galilean satellites, with the aid of both earth-based radio and on-board video data.
Russell, R. K.↗
Galileo satellite tour maneuver strategies
In January of 1982 the United States will launch Galileo, the first space mission designed to perform an intensive tour of the Galilean satellites of Jupiter. This paper discusses the results of preliminary maneuver strategy studies for typical interplanetary and orbital phases of the Galileo mission. These studies include the effects of maneuver placement and various linear control algorithms on propellant consumption as determined by Monte Carlo analysis. Estimates of total propellant required for various probabilities of mission success are also given.
Miller, L. J.↗
Voyager 2 - A grand tour of the giant planets
The current Voyager 2 multiple gravity assist mission encountering Jupiter, Saturn, Uranus and Neptune is reviewed. Included in the discussion are an historical background of the mission, emphasizing objectives and constraints, and the mission synthesis and selection for the Saturn, Uranus and Neptune encounters. The philosophy, options, characteristics and constraints of the encounters are also discussed, including the avoidance of rings, penetration into magnetic fields, and date synchronization. In addition, the trajectory selection process which resulted in the choice of the specific outer planet tour is summarized, and current reevaluations are presented.
Sergeyevsky, A. B.↗
The design of sport and touring aircraft
General considerations concerning the design of a new aircraft are discussed, taking into account the objective to develop an aircraft can satisfy economically a certain spectrum of tasks. Requirements related to the design of sport and touring aircraft included in the past mainly a high cruising speed and short take-off and landing runs. Additional requirements for new aircraft are now low fuel consumption and optimal efficiency. A computer program for the computation of flight performance makes it possible to vary automatically a number of parameters, such as flight altitude, wing area, and wing span. The appropriate design characteristics are to a large extent determined by the selection of the flight altitude. Three different wing profiles are compared. Potential improvements with respect to the performance of the aircraft and its efficiency are related to the use of fiber composites, the employment of better propeller profiles, more efficient engines, and the utilization of suitable instrumentation for optimal flight conduction.
Eppler, R.↗