Independence-X Aerospace

Last updated

Independence-X Aerospace
Type Private Limited Company
Industry Aerospace
Launch service provider
Founded2013;9 years ago (2013)
FounderIzmir Yamin
Headquarters,
Key people
ProductsCryogenic rocket engine
Dedicated Nano Launch Vehicle (DNLV)
Microgravity Experiment Re-entry Capsule (MERCAP)
Hall-effect thruster
Website independence-x.com

Independence-X Aerospace or better known as IDXA is a NewSpace Transportation Systems company based in Seremban, Malaysia. It provides Microgravity Experiment Re-entry Capsule Service, Launch Services, Low-Cost Satellite Development and Launch, Ground Station Service, and aims for Interplanetary Missions.

Contents

History

Independence-X Aerospace or IDXA was founded in 2013 by Founder, CEO and CTO Izmir Yamin and based in Seremban, Malaysia. Back then, the initiatives was parked under a Special Interest Group experimenting with different rocket technology at engineering model and lab scale, which led to the state of the art technology on its feeding system which can reduce the entire mass of existing feeding system for liquid propellant technology by half and less the power consumption. This discovery will later help to translate into better cost effective launch price for future customers. Having the added advantage of being an equatorial launcher, it makes DNLV (Dedicated Nano Launch Vehicle) the preferred future launch for small, pico and nano class satellites.

Since 2003, three different engineering models had been designed, built and test flight which achieved remarkable success where it also won Gold Medals in Europe for its innovativeness. The rocket motor and engines are as follows: ID-1 (Solid Propellant Rocket Motor, 2003), ID-2 (Upgraded version - Solid Propellant Rocket Motor, 2005), ID-3 (Liquid Propellant Rocket Engine, 2006).

Current development

Commercial nano satellite launcher

IDXA would be providing future commercial rocket launch services into Low Earth Orbit (LEO). The rocket launcher is known as the Dedicated Nano Launch Vehicle (DNLV) to be commercial ready by 2025, [1] which was featured in NASA "Small Spacecraft Technology: State of the Art" December 2015 report. [2] The DNLV is capable of providing dedicated launch services to small satellites and cubesat owners for insertion into their intended orbit and inclination. IDXA is looking at frequent launches from near equatorial launch site for at least twice a month for the first year (24 launches / year). DNLV is capable of delivering payloads of 200 kg to a 500 km Sun-synchronous orbit (SSO).

Interplanetary mission

Interplanetary mission is currently being planned for post the year 2020, where IDXA is developing a bio-mimetic flapping winged micro aerial vehicle (B-MAV) robotic dragonfly to scout the Martian Surface to assist NASA's future Mars rover from the rough rocky Martian terrain to perform ground exploration much easily by providing avoidable obstacle path.

Re-entry capsule

IDXA is also developing a Microgravity Experiment Re-entry Capsule (MERCAP) in the pipeline for future commercial missions. [3]

See also

Related Research Articles

<span class="mw-page-title-main">Interplanetary spaceflight</span> Crewed or uncrewed travel between stars or planets

Interplanetary spaceflight or interplanetary travel is the crewed or uncrewed travel between stars and planets, usually within a single planetary system. In practice, spaceflights of this type are confined to travel between the planets of the Solar System. Uncrewed space probes have flown to all the observed planets in the Solar System as well as to dwarf planets Pluto and Ceres, and several asteroids. Orbiters and landers return more information than fly-by missions. Crewed flights have landed on the Moon and have been planned, from time to time, for Mars and Venus. While many scientists appreciate the knowledge value that uncrewed flights provide, the value of crewed missions is more controversial. Science fiction writers propose a number of benefits, including the mining of asteroids, access to solar power, and room for colonization in the event of an Earth catastrophe.

<span class="mw-page-title-main">Mariner program</span> NASA space program from 1962 to 1973

The Mariner program was conducted by the American space agency NASA to explore other planets. Between 1962 and late 1973, NASA's Jet Propulsion Laboratory (JPL) designed and built 10 robotic interplanetary probes named Mariner to explore the inner Solar System - visiting the planets Venus, Mars and Mercury for the first time, and returning to Venus and Mars for additional close observations.

<span class="mw-page-title-main">Spacecraft propulsion</span> Method used to accelerate spacecraft

Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites. In-space propulsion exclusively deals with propulsion systems used in the vacuum of space and should not be confused with space launch or atmospheric entry.

<span class="mw-page-title-main">Spaceflight</span> Flight into or through outer space

Spaceflight is an application of astronautics to fly spacecraft into or through outer space, either with or without humans on board. Most spaceflight is uncrewed and conducted mainly with spacecraft such as satellites in orbit around Earth, but also includes space probes for flights beyond Earth orbit. Such spaceflight operates either by telerobotic or autonomous control. The more complex human spaceflight has been pursued soon after the first orbital satellites and has reached the Moon and permanent human presence in space around Earth, particularly with the use of space stations. Human spaceflight programs include the Soyuz, Shenzhou, the past Apollo Moon landing and the Space Shuttle programs, with currently the International Space Station as the main destination of human spaceflight missions while China's Tiangong Space Station is under construction.

<span class="mw-page-title-main">CubeSat</span> Miniature satellite in 10cm cube modules

A CubeSat is a class of miniaturized satellite based around a form factor consisting of 10 cm (3.9 in) cubes. CubeSats have a mass of no more than 2 kg (4.4 lb) per unit, and often use commercial off-the-shelf (COTS) components for their electronics and structure, some non for profit organizations such as KSF Space Foundation offering cheapest on shelf cubesat kit as well. CubeSats are put into orbit by deployers on the International Space Station, or launched as secondary payloads on a launch vehicle. As of August 2021, more than 1,600 CubeSats have been launched.

<span class="mw-page-title-main">JAXA</span> Japans national air and space agency

The Japan Aerospace Exploration Agency (JAXA) is the Japanese national air and space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and launch of satellites into orbit, and is involved in many more advanced missions such as asteroid exploration and possible human exploration of the Moon. Its motto is One JAXA and its corporate slogan is Explore to Realize.

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<span class="mw-page-title-main">Aerocapture</span> Orbital transfer maneuver

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<span class="mw-page-title-main">Space Capsule Recovery Experiment</span>

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<span class="mw-page-title-main">Orbital propellant depot</span> Cache of propellant that is placed in orbit to allow spacecraft to refuel in space

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<span class="mw-page-title-main">Orbiting Vehicle</span> American satellite family

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<span class="mw-page-title-main">NASA Launch Services Program</span>

The NASA Launch Services Program (LSP) is responsible for procurement of launch services for NASA uncrewed missions and oversight of launch integration and launch preparation activity, providing added quality and mission assurance to meet program objectives. LSP operates under the NASA Space Operations Mission Directorate (SOMD).

<span class="mw-page-title-main">Cygnus Orb-3</span> Failed 2014 American resupply spaceflight to the ISS

Orbital-3, also known as Orb-3, was an attempted flight of Cygnus, an automated cargo spacecraft developed by United States-based company Orbital Sciences, on 28 October 2014. The mission was intended to launch at 22:22:38 UTC that evening. This flight, which would have been its fourth to the International Space Station and the fifth of an Antares launch vehicle, resulted in the Antares rocket exploding seconds after liftoff.

SLOSHSAT-FLEVO is a microsatellite launched to investigate the dynamics of fluids in microgravity. FLEVO stands for Facility for Liquid Experimentation and Verification in Orbit. Multiple sensors were used to monitor the behavior of water in an instrumented tank and how sloshing affects the attitude control of launchers and space vehicles.

<span class="mw-page-title-main">Green Propellant Infusion Mission</span> NASA satellite testing a new rocket fuel

The Green Propellant Infusion Mission (GPIM) was a NASA technology demonstrator project that tested a less toxic and higher performance/efficiency chemical propellant for next-generation launch vehicles and CubeSat spacecraft. When compared to the present high-thrust and high-performance industry standard for orbital maneuvering systems, which for decades, have exclusively been reliant upon toxic hydrazine based propellant formulations, the "greener" hydroxylammonium nitrate (HAN) monopropellant offers many advantages for future satellites, including longer mission durations, additional maneuverability, increased payload space and simplified launch processing. The GPIM was managed by NASA's Marshall Space Flight Center in Huntsville, Alabama, and was part of NASA's Technology Demonstration Mission Program within the Space Technology Mission Directorate.

<span class="mw-page-title-main">OV1-1</span> US Air Force satellite

Orbiting Vehicle 1-1, was the first satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-1 was an American Earth science research satellite designed to measure radiation, micrometeoroid density, and magnetic fields in orbit. Launched 21 January 1965, the mission resulted in failure when, after a successful launch of its Atlas booster, OV1-1's onboard Altair motor failed to fire.

<span class="mw-page-title-main">OV2-3</span> US Air Force satellite

Orbiting Vehicle 2-3, the second satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American solar astronomy, geomagnetic and particle science research satellite. Launched 22 December 1965 along with three other satellites, the mission resulted in failure when the spacecraft failed to separate from the upper stage of its Titan IIIC.

<span class="mw-page-title-main">OV1-4</span> US Air Force satellite

Orbiting Vehicle 1-4, launched 30 Mar 1966, was the fourth, and second successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-4 was a long-term bioscience and materials science satellite, designed to return data relevant to long-term human presence in space. Its launch marked the first time two satellites were placed into orbit side by side with each other.

References

  1. "Dedicated Nano Launch Vehicle (DNLV)" . Retrieved 16 August 2022.
  2. "Small Spacecraft Technology State of the Art" (PDF). NASA . Retrieved 31 December 2015.
  3. "Re-entry Capsule - Independence-X Aerospace". IDXA. Retrieved 16 August 2022.