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* Spacecraft propulsion — Other methods of spacecraft propulsion used to change the velocity of spacecraft and artificial satellites.
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Spacecraft and propulsion
* Spacecraft propulsion engines such as Rocket engine
* Spacecraft propulsion
# REDIRECT Spacecraft propulsion
* Spacecraft propulsion — describes many different propulsion systems for spacecraft
# REDIRECT Spacecraft propulsion
** Spacecraft propulsion
Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites.
* Spacecraft propulsion
Category: Spacecraft propulsion
Category: Spacecraft propulsion
Category: Spacecraft propulsion
* Spacecraft propulsion
Category: Spacecraft propulsion
A resistojet is a method of Spacecraft propulsion ( Electric propulsion ) that provides thrust by heating a ( typically non-reactive ) fluid.
Category: Spacecraft propulsion
Category: Spacecraft propulsion
Category: Spacecraft propulsion
* Spacecraft propulsion
Category: Spacecraft propulsion
Category: Spacecraft propulsion
* Spacecraft propulsion
* Spacecraft propulsion
* Spacecraft propulsion
Spacecraft and —
* System F6 — a DARPA Fractionated Spacecraft demonstrator
:" Spacecraft 107 — alias Apollo 11 — alias Columbia.
Spacecraft —
Spacecraft propulsion —
Spacecraft and Other
Other American manned spacecraft include the Gemini Spacecraft, Apollo Spacecraft, the Skylab space station, and the Space Shuttle with undetached European Spacelab and private US Spacehab space stations-modules.
Spacecraft and spacecraft
Spacecraft subsystems comprise the spacecraft " bus " and may include: attitude determination and control ( variously called ADAC, ADC or ACS ), guidance, navigation and control ( GNC or GN & C ), communications ( Comms ), command and data handling ( CDH or C & DH ), power ( EPS ), thermal control ( TCS ), propulsion, and structures.
; Power: Spacecraft need an electrical power generation and distribution subsystem for powering the various spacecraft subsystems.
Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites.
Spacecraft with instruments whose primary purpose is to provide data for space weather predictions and applications include the GOES series of spacecraft, the POES series, the DMSP series, and the Meteosat series.
* Fuji ( Spacecraft ), a capsule type manned spacecraft concept, proposed by NASDA
Later his student Robert R. Gilruth, who became the director of the NASA Manned Spacecraft Center, approved and used them in spacecraft.
To maintain low costs, the spacecraft incorporated many designs and technologies used in past missions or previously developed for future missions by the Small Spacecraft Technologies Initiative ( SSTI ).
The solar array design was derived primarily from the Small Spacecraft Technology Initiative ( SSTI ) spacecraft development guidelines.
* Spacecraft propulsion: how spacecraft change orbits, and how they are launched.
Young atop a Gemini spacecraft with Grissom in the water at left at the Manned Spacecraft Center during water egress training
Spacecraft # 11 was the first Mercury operational spacecraft with a centerline window.
In 1994, the Panel on Small Spacecraft Technology was established to set guidelines for future miniature spacecraft.
Spacecraft include optical reconnaissance satellites, communications satellites, early warning missile defence spacecraft, nuclear-powered radar reconnaissance satellites, anti-satellite weapons and their targets, navigation satellites and technology demonstrators.
Complete Apollo spacecraft: Command Module, Service Module, Lunar Module, Launch Escape System, Spacecraft LM Adapter
Two additional components complemented the spacecraft stack for launch vehicle assembly: a Launch Escape System ( LES ) to be used only in the event of a launch emergency, and a Spacecraft / Lunar Module Adapter ( SLA ) designed to connect the CSM to the launch vehicle and to house the LM.
Spacecraft Event Time ( SCET ) is the time an event occurs at a spacecraft.
The Spacecraft Event Time of a singular event on the spacecraft can also be defined as equal to the ERT ( Earth-Received Time ) minus the OWLT ( One-Way Light Time ), or as TRM ( transmission time ) plus OWLT.
William Wollenhaupt and Emil Schiesser of the NASA Manned Spacecraft Center in Houston then worked out the " fix " that was first applied to Apollo 12 and permitted its landing within 163 meters of the target, the previously-landed Surveyor 3 spacecraft.
Prior assignments at RCA included Integration and Test Manager for the Satcom D & E spacecraft, responsible for implementation of all launch site activities, and Spacecraft Bus Manager on the Spacenet / Gstar programs, responsible for satisfaction of multiple launch vehicle interfaces ( Delta, STS and Ariane ) by the spacecraft bus design.
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