With the advent of the manned space station, man now requires a spacecraft based on the space station with the ability to deploy, recover, and repair satellites quickly and economically. Such a craft would prolong and enhance the life and performance of many satellites. A basic design was developed for an orbital tansfer vehicle (OTV). The basic design criteria are discussed. The design of the OTV and systems were researched in the following areas: avionics, crew systems, electrical power systems, environmental control/life support systems, navigation and orbital maneuvers, propulsion systems, reaction control systems (RCS), servicing systems, and structures. The basic concepts in each of the areas are summarized
Three groups of student engineers in an aerospace vehicle design course present their designs for a ...
The most optimal design for a chemical propellant, manned OTV that fulfills the described constraint...
Mars transfer vehicles (MTV\u27s) using nuclear thermal propulsion (NTP) to reduce transit time intr...
The Orbital Transfer Vehicle (OTV) and systems were researched in the following areas: avionics, cre...
The expended capabilities for Orbital Transfer Vehicles (OTV) which will be needed to meet increased...
A new Orbital Transfer Vehicle (OTV) propulsion system that will be used in conjunction with the Spa...
The design of an unmanned, space-based, reusable Orbital Transfer Vehicle (OTV) is presented. This O...
Studies of the United States Space Transportation System show that in the mid-to-late 1990s expanded...
The objectives of the Phase 2 study were to improve the orbit transfer vehicle (OTV) concept definit...
This portion of the Orbit Transfer Vehicle (OTV) Concept Definition and System Analysis Study, Volum...
The key system and program trade studies performed to arrive at a preferred Orbital Transfer Vehicle...
Space based servicing of an orbit transfer vehicle (OTV) was previously outlined in sufficient detai...
A reuseable orbit transfer vehicle concept was defined and subsequent recommendations for the design...
The major technology issues for an advanced orbital transfer vehicles (OTV) engine to be used in con...
The basic components of the design for the orbital transfer vehicle (OTV) are outlined. The Project ...
Three groups of student engineers in an aerospace vehicle design course present their designs for a ...
The most optimal design for a chemical propellant, manned OTV that fulfills the described constraint...
Mars transfer vehicles (MTV\u27s) using nuclear thermal propulsion (NTP) to reduce transit time intr...
The Orbital Transfer Vehicle (OTV) and systems were researched in the following areas: avionics, cre...
The expended capabilities for Orbital Transfer Vehicles (OTV) which will be needed to meet increased...
A new Orbital Transfer Vehicle (OTV) propulsion system that will be used in conjunction with the Spa...
The design of an unmanned, space-based, reusable Orbital Transfer Vehicle (OTV) is presented. This O...
Studies of the United States Space Transportation System show that in the mid-to-late 1990s expanded...
The objectives of the Phase 2 study were to improve the orbit transfer vehicle (OTV) concept definit...
This portion of the Orbit Transfer Vehicle (OTV) Concept Definition and System Analysis Study, Volum...
The key system and program trade studies performed to arrive at a preferred Orbital Transfer Vehicle...
Space based servicing of an orbit transfer vehicle (OTV) was previously outlined in sufficient detai...
A reuseable orbit transfer vehicle concept was defined and subsequent recommendations for the design...
The major technology issues for an advanced orbital transfer vehicles (OTV) engine to be used in con...
The basic components of the design for the orbital transfer vehicle (OTV) are outlined. The Project ...
Three groups of student engineers in an aerospace vehicle design course present their designs for a ...
The most optimal design for a chemical propellant, manned OTV that fulfills the described constraint...
Mars transfer vehicles (MTV\u27s) using nuclear thermal propulsion (NTP) to reduce transit time intr...