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This document describes the format and contents of the archive volume housing HiRISE Standard products, including Experiment Data Record (EDR) and Reduced Data Records (RDR) Products, detailing the
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How to fill out Mars Reconnaissance Orbiter HiRISE Software Interface Specification

01
Gather all necessary documentation and prerequisites for the Mars Reconnaissance Orbiter HiRISE project.
02
Familiarize yourself with the specifications and requirements outlined in the existing HiRISE documentation.
03
Use the provided templates and forms to structure your input.
04
Fill out the software interface specification with accurate information, following the guidelines for each section.
05
Clearly define the software functionalities and interfaces required for interacting with HiRISE data.
06
Review and validate the filled-out specification against the project's objectives and requirements.
07
Submit the completed specification for review by team leads or project managers.

Who needs Mars Reconnaissance Orbiter HiRISE Software Interface Specification?

01
Software developers working on HiRISE-related applications.
02
Project managers overseeing Mars reconnaissance missions.
03
Researchers utilizing HiRISE data for scientific analysis.
04
Quality assurance teams reviewing software compliance with specifications.
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People Also Ask about

HiRISE (High Resolution Imaging Science Experiment) is the most powerful camera ever sent to another planet, one of six instruments onboard the Mars Reconnaissance Orbiter. We launched in 2005, arrived at Mars in 2006 and have been imaging ever since.
There are four main types of science instruments on the rover: (1) the contact instruments APXS (Alpha-Particle X-ray Spectrometer) and MAHLI (Mars Hand Lens Imager) on the end of the robotic arm; (2) the remote sensing instruments ChemCam (Chemical Camera) and Mastcam (Mast Cameras) mounted on the mast; (3) the
As of July 29, 2023, the MRO has returned over 450 terabits of data, helped choose safe landing sites for NASA's Mars landers, discovered pure water ice in new craters and further evidence that water once flowed on the surface on Mars. The spacecraft continues to operate at Mars, far beyond its intended design life.
In addition, there are three engineering instruments aboard MRO: the Electra UHF communications and navigation package, which will be used as a relay between the Earth and future Mars missions; the optical navigation camera, which will be tested for possible navigational use on future planetary spacecraft; and the Ka-
MRO has 20 rocket engine thrusters on board. Six large thrusters each produce 170 N (38 lbf) of thrust for a total of 1,020 N (230 lbf) meant mainly for orbital insertion. These thrusters were originally designed for the Mars Surveyor 2001 Lander.
The spacecraft encountered Mars on a trajectory that brought it too close to the planet, and it was destroyed in the atmosphere. An investigation attributed the failure to a measurement mismatch between two measurement systems: SI units (metric) by NASA and US customary units by spacecraft builder Lockheed Martin.
From an altitude that varies from about 125 to 250 miles (200 to 400 kilometers) above Mars, HiRISE acquires surface images containing individual, basketball-size (1 to 2 feet, or 30 to 60 centimeters), pixel elements, allowing surface features 4 to 8 feet (about 1.3 to 2.4 meters) across to be resolved.

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The Mars Reconnaissance Orbiter HiRISE Software Interface Specification is a formal document that outlines the requirements, functionality, and protocols for software interfaces used in the HiRISE (High Resolution Imaging Science Experiment) imaging system aboard the Mars Reconnaissance Orbiter.
Individuals or teams involved in the development, integration, or use of software systems that interact with the HiRISE imaging system are required to file this specification.
To fill out the specification, users must complete the designated sections detailing the software capabilities, operational parameters, data interfaces, and any relevant compliance requirements in accordance with provided guidelines.
The purpose of the specification is to ensure interoperability, facilitate communication, and define the requirements for integrating and utilizing software with the HiRISE imaging system effectively.
The specification must report information such as software versioning, interface functionalities, data formats, error handling protocols, and compatibility with existing systems.
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