Lunar Reconnaissance Orbiter Project Technical Resource
... Nutation Time Constant (NTC). The overall mass allocation did not change since the launch vehicle capability remained the same. The project has now settled on using an Evolved expendable launch vehicle (EELV) verses an intermediate class launch vehicle (Delta-IV or Altas-5) per Headquarters’ (HQ) di ...
... Nutation Time Constant (NTC). The overall mass allocation did not change since the launch vehicle capability remained the same. The project has now settled on using an Evolved expendable launch vehicle (EELV) verses an intermediate class launch vehicle (Delta-IV or Altas-5) per Headquarters’ (HQ) di ...
gesis FLEX - Wieland Electric Canada
... Because of the flat shape, the connection from one side, well-thought-out mounting options and the modular concept of this system fits in almost any space. The strictly pluggable design allows a fast, secure, and simple connection. The manual control directly on the modules simplifies start-up and t ...
... Because of the flat shape, the connection from one side, well-thought-out mounting options and the modular concept of this system fits in almost any space. The strictly pluggable design allows a fast, secure, and simple connection. The manual control directly on the modules simplifies start-up and t ...
I PowerFilm® Module Polarity Information II PowerFilm® Module
... Charging Batteries: Current Second, select the appropriate Operating Current of the solar module to charge your load. As a general rule, do not charge a rechargeable battery with more current than 10% of its rated capacity. For example, a 700mA-hour battery can be safely charged with a solar module ...
... Charging Batteries: Current Second, select the appropriate Operating Current of the solar module to charge your load. As a general rule, do not charge a rechargeable battery with more current than 10% of its rated capacity. For example, a 700mA-hour battery can be safely charged with a solar module ...
Instruction Manual
... are not guaranteed. In accordance with Cooper Crouse-Hinds "Terms and Conditions of Sale," and since conditions of use are outside our control, the purchaser should determine the suitability of the product for his intended use and assumes all risk and liability whatsoever in connection therewith. ...
... are not guaranteed. In accordance with Cooper Crouse-Hinds "Terms and Conditions of Sale," and since conditions of use are outside our control, the purchaser should determine the suitability of the product for his intended use and assumes all risk and liability whatsoever in connection therewith. ...
Albert Caubet
... • Absolute reference position using computer vision system on-board chaser – use chaser’s attitude sensors • Specially relevant for autonomous propulsive approach – Guidance and Navigation take place in the chaser ...
... • Absolute reference position using computer vision system on-board chaser – use chaser’s attitude sensors • Specially relevant for autonomous propulsive approach – Guidance and Navigation take place in the chaser ...
Initial observations from the Lunar Orbiter Laser Altimeter (LOLA)
... 30 km × 216 km polar orbit, with periapsis near the south pole. During this spacecraft‐commissioning phase, the performance of the spacecraft and the instruments was validated and instrument calibrations were performed. LOLA was turned on for an initial check on July 3, 2009 for two days and both la ...
... 30 km × 216 km polar orbit, with periapsis near the south pole. During this spacecraft‐commissioning phase, the performance of the spacecraft and the instruments was validated and instrument calibrations were performed. LOLA was turned on for an initial check on July 3, 2009 for two days and both la ...
this page
... to the moon was worth the risks. It would be like a "Hail, Mary" pass during the closing seconds of a football game for the win. Chief rocket engineer Wernher von Braun assured him that the powerful Saturn V moon rocket would work despite previous setbacks; the rocket had never been tested with a ma ...
... to the moon was worth the risks. It would be like a "Hail, Mary" pass during the closing seconds of a football game for the win. Chief rocket engineer Wernher von Braun assured him that the powerful Saturn V moon rocket would work despite previous setbacks; the rocket had never been tested with a ma ...
Apollo Lunar Module
The Apollo Lunar Module (LM), originally designated the Lunar Excursion Module (LEM), was the lander portion of the Apollo spacecraft built for the US Apollo program by Grumman Aircraft to carry a crew of two from lunar orbit to the surface and back. Designed for lunar orbit rendezvous, it consisted of an ascent stage and descent stage, and was ferried to lunar orbit by its companion Command and Service Module (CSM), a separate spacecraft of approximately twice its mass, which also took the astronauts home to Earth. After completing its mission, the LM was discarded. It was capable of operation only in outer space; structurally and aerodynamically it was incapable of flight through the Earth's atmosphere. The Lunar Module was the first, and to date only, manned spacecraft to operate exclusively in the airless vacuum of space.Six such craft successfully landed on the Moon between 1969 and 1972. A seventh provided propulsion and life support for the crew of Apollo 13 when their CSM was disabled by an oxygen tank explosion en route to the Moon.The LM's development was plagued with problems which delayed its first unmanned flight by about ten months, and its first manned flight by about three months. Despite this, the LM eventually became the most reliable component of the Apollo/Saturn space vehicle, the only component never to suffer a failure that significantly impacted a mission. It holds the distinction of being the first, and to date only, manned vehicle to either land on or take off from a natural object in the solar system other than the Earth.