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A KC-135 Stratotanker aircraft flight simulator during

STS082-730-012 - STS-082 - HST, survey of the telescope -V3 side

OA-7 Service Module Arrival. NASA public domain image. Kennedy space center.

KENNEDY SPACE CENTER, FLA. -- The Dawn spacecraft is seen here in clean room C of Astrotech's Payload Processing Facility. In the clean room, the spacecraft will undergo further processing. Dawn's mission is to explore two of the asteroid belt's most intriguing and dissimilar occupants: asteroid Vesta and the dwarf planet Ceres. The Dawn mission is managed by JPL, a division of the California Institute of Technology in Pasadena, for NASA's Science Mission Directorate in Washington, D.C. Photo credit: NASA/George Shelton KSC-07pd0864

TEKA0006299, Tekniska museet, Sweden

KENNEDY SPACE CENTER, FLA. -- Technicians at Astrotech prepare the Dawn spacecraft for spin-balance testing. After the test, Dawn will then be mated to the upper stage booster, installed into a spacecraft transportation canister for the trip to Cape Canaveral Air Force Station and mated to the Delta II rocket at Launch Pad 17-B. The Dawn spacecraft will employ ion propulsion to explore two of the asteroid belt's most intriguing and dissimilar occupants: asteroid Vesta and the dwarf planet Ceres. Dawn's goal is to characterize the conditions and processes of the solar system's earliest epoch by investigating in detail these largest protoplanets that have remained intact since their formations. Ceres and Vesta reside in the extensive zone between Mars and Jupiter together with many other smaller bodies, called the asteroid belt. Dawn is scheduled to launch July 7. Photo credit: NASA/Jack Pfaller KSC-07pd1505

Early Program Development. NASA public domain image colelction.

Environmental Testing - NASA Rover images

STS082-731-011 - STS-082 - HST, survey views of the telescope surface and structures

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Mars 1. NASA public domain image colelction.

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Summary

Description: (November 1, 1962) Mars 1 was an automatic interplanetary station launched in the direction of Mars, with the intent of flying by the planet at a distance of about 11,000 km. It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. ..After leaving Earth orbit, the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at 5 days in which a large amount of interplanetary data were collected. ..On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars communications ceased, probably due to failure of the spacecraft orientation system. Mars 1 closest approach to Mars occurred on 19 June 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit.

NASA Photo Collection

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mars mars 1 1962 spacecraft distance spacecraft orientation system mars communications data earth orbit orientation system two day intervals radiation environment sixty one radio transmissions radiation micrometeoroid impacts earth orbit gas valves gyroscopic stabilization satellite nasa
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1962
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label_outline Explore Mars 1, Radiation, 1962

A detailed view of the weapons load of an F-16C Falcon from the 52nd Fighter Wing based at Spandahlem AB Germany as it takes on fuel from a 100th Air Expeditionary Wing KC-135R Stratotanker (not shown) from RAF Mildenhall United Kingdom on 31 Mar 99. While patroling the skies over Kosovo during Operation Allied Force, it is armed with AIM-120C missiles on the two outboard stations for self protection and Highspeed Anti Radiation Missiles on the inboard station to suppress anti-aircraft radar sites

S107E05736 - STS-107 - Chawla enters data on a laptop computer for the SOFBALL experiment in the SH during STS-107

S117E07236 - STS-117 - Swanson prepares to retract the P6 Truss STBD SAW during EVA 2

STS063-25-015 - STS-063 - SPACEHAB and the IMAX camera in Discovery's payload bay

STS069-719-013 - STS-069 - Wake Shield Facility in orbit above the Earth

Steve Highly, left, Jim Hollinger, center, and Allen Rose calibrate SSM/I radiometers in the Image Processing Facility at the Naval Research Laboratory (NRL). Radiometers mounted aboard a RP-3A Orion aircraft will be used to validate data obtained through the Defense Meteorological Satellite Program (DMSP), a joint Navy/Air Force project

STS070-702-035 - STS-070 - Deploy of Tracking and Data Relay Satellite G (TDRS-G)

STS109-729-070 - STS-109 - Distant views of Hubble over Earth Limb after redeploy

S112E05853 - STS-112 - Flyaround data on laptop computer

F-100 FAILURE DATA, NASA Technology Images

STS103-374-027 - STS-103 - Various views of the HST after release

S126E008929 - STS-126 - Bowen during EVA 3

Topics

mars mars 1 1962 spacecraft distance spacecraft orientation system mars communications data earth orbit orientation system two day intervals radiation environment sixty one radio transmissions radiation micrometeoroid impacts earth orbit gas valves gyroscopic stabilization satellite nasa