Instrument Pointing Subsystem requirements for Spacelab missions in solar physics, stellar astronomy, and earth observation are analyzed and design guidelines for fine pointing instrument platforms are presented. The requirements for the platforms are time-phased based on NASA projections of flight mission models and payload scheduling. The experiments used for these projections are to be viewed as representative payloads. Other experiments or experiment groupings within any one discipline may be accommodated by an Instrument Pointing Subsystem that meets these requirements
This article addresses the role of man in operating on orbit a large pointing system such as the IPS...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...
This paper describes the Annular Suspension and Pointing System (ASPS) being developed to support NA...
The goal of the experiment pointing subsystems (EPS) is to accommodate a broad spectrum of instrumen...
Surveys of potential space station astrophysics payload requirements and existing point mount design...
This paper reports the performance of the Instrument Pointing System (IPS) that flew on the National...
The Kennedy launch site capability for accommodating spacelab payload operations was assessed. Anoma...
Technology assessment is performed for pointing systems that accommodate payloads of large mass and ...
Suitability of support and test equipment from the UARS Spacecraft Solar Stellar Pointing Platform (...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
The shuttle orbiter inertial measurement unit (IMU), located in the orbiter cabin, is used to supply...
Preliminary error budgets for the pointing knowledge, control, and stability of the SIM spacecraft a...
The conditions for absorption spectroscopy of the homosphere between 20 and 100 km from a space plat...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
This article addresses the role of man in operating on orbit a large pointing system such as the IPS...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...
This paper describes the Annular Suspension and Pointing System (ASPS) being developed to support NA...
The goal of the experiment pointing subsystems (EPS) is to accommodate a broad spectrum of instrumen...
Surveys of potential space station astrophysics payload requirements and existing point mount design...
This paper reports the performance of the Instrument Pointing System (IPS) that flew on the National...
The Kennedy launch site capability for accommodating spacelab payload operations was assessed. Anoma...
Technology assessment is performed for pointing systems that accommodate payloads of large mass and ...
Suitability of support and test equipment from the UARS Spacecraft Solar Stellar Pointing Platform (...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
The shuttle orbiter inertial measurement unit (IMU), located in the orbiter cabin, is used to supply...
Preliminary error budgets for the pointing knowledge, control, and stability of the SIM spacecraft a...
The conditions for absorption spectroscopy of the homosphere between 20 and 100 km from a space plat...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
This article addresses the role of man in operating on orbit a large pointing system such as the IPS...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.In...
This paper describes the Annular Suspension and Pointing System (ASPS) being developed to support NA...