Micro-Space

Last updated
Micro-Space
FormerlySpectron Instrument Corporation
Industry Aerospace
FoundedFebruary 1977 (1977-02) in Denver, Colorado, USA
FounderRichard P. Speck
Defunct2011 (2011)
FateDissolved
Headquarters,

Micro-Space was an aerospace corporation based in Denver, Colorado, founded in February 1977 by Richard P. Speck under the name Spectron Instrument Corporation. The corporation changed its name to "Micro-Space, Inc." in 1998. It was dissolved in 2011, following the death of the founder.

Contents

In addition to funding and building a number of its own spacecraft and rockets, Micro-Space was a component supplier to the emerging [1] CubeSat industry. [2]

Philosophy

Micro-Space operated using a strategy based on using modern technology to achieve radical downsizing of space systems to minimize launch cost and make mission financing feasible. They claim cost-effectiveness is maximised by creating satellites the size of lunchboxes and cell phones as opposed to "Volkswagens".

History

While one of the smaller teams participating in the Ansari X Prize competition, Micro-Space had previously developed an active aerospace program flying innovative liquid fueled rockets. A long history of flying small rockets with telemetry, tracking and control systems demonstrates its focus on the fundamental systems necessary for uncrewed - and eventually crewed - suborbital and orbital launch vehicle and satellite systems. [2] While its operational systems are most appropriate for atmospheric research, the company claims to have produced modules which, if clustered, could power a "spartan" crewed launch.[ citation needed ]

Seventeen liquid fueled, bipropellant rockets were successfully flown by 2006, with altitudes to 11,000 feet. Hydrogen peroxide and methyl alcohol were the fuels.[ citation needed ]

Micro-Space competed in the 2006 Lunar Lander Challenge held in Las Cruces, New Mexico, part of the Centennial Challenges competitions sponsored by NASA, and was considered by event organizers as one of two favorites to win. [3]

Micro-Space also built operational prototypes suitable for long duration life support and other needs of lunar and interplanetary missions, including Mars landing. The company was dissolved in 2011. [4]

Micro-Space was manifested to fly two CubeSats on a "Ride Sharing" launch with EduSAT, Sich-2 and other spacecraft, to be flown on a Dnepr rocket into a near-polar Sun-synchronous orbit in October 2010. Payload integration for this satellite group was handled by Morehead State University, involving Dr. Ben Malphrus (Space Science Center director) and professor Bob Twiggs. Micro-Space also planned to deliver two similar spacecraft to Morehead State and the University of Colorado at Colorado Springs. [5]

The complete, four satellite "PQ-Gemini ++" mission group, in addition to validating general satellite systems, was to be capable of demonstrating Micro-Space interferometric techniques to characterize orbital differences using only precision range data between ultralight spacecraft in preparation for autonomous rendezvous. Additional systems were to allow the relative positions, distance and rotational alignment of the four satellites to be continuously monitored. This information is necessary for the final, docking procedures. Other developmental steps were projected to follow, leading to ultralight sample return missions on the Moon and Mars.[ needs update ]

In 2010 Micro-space was selected to negotiate a NASA Phase I SBIR contract entitled "Non-Radiated Field Link to Recharge, Reprogram, Test and Co-ordinate Aux. Payload Systems". Unfortunately, the untimely death of Richard P. Speck in October 2010 effectively halted all programs.

In 2007, Micro-Space was discussing return sample analysis and lunar prospecting with several organizations. [6] Prospecting operations will be aimed at locating concentrations of extractable lunar gems and minerals. High grade titanium, rare-earth metals and helium-3 (a potential fusion reactor fuel) are all known to exist on the Moon. Low cost flight of concentrated ores to the Earth is feasible using Solar Powered, electromagnetic "Rail guns", and other technologies.[ citation needed ]

Propellant to complete rendezvous and docking was not allowed in the planned satellite cluster launch. Arrangements were being negotiated for launch 2011 of small Micro-Space spacecraft with propulsion systems to demonstrate the complete rendezvous and docking process as will be used with “Planetary Ascent Vehicles” carrying prospecting samples. Negotiations with this launch supplier also cover subsequent launch of a “Lunar Lander” and Lunar Transfer spacecraft, as well as the Planetary Ascent and Return vehicles.[ citation needed ]

Related Research Articles

<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. 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">Small satellite</span> Satellites of low mass and size, usually under 500 kg

A small satellite, miniaturized satellite, or smallsat is a satellite of low mass and size, usually under 1,200 kg (2,600 lb). While all such satellites can be referred to as "small", different classifications are used to categorize them based on mass. Satellites can be built small to reduce the large economic cost of launch vehicles and the costs associated with construction. Miniature satellites, especially in large numbers, may be more useful than fewer, larger ones for some purposes – for example, gathering of scientific data and radio relay. Technical challenges in the construction of small satellites may include the lack of sufficient power storage or of room for a propulsion system.

<span class="mw-page-title-main">Orbital propellant depot</span> Cache of propellant used to refuel spacecraft

An orbital propellant depot is a cache of propellant that is placed in orbit around Earth or another body to allow spacecraft or the transfer stage of the spacecraft to be fueled in space. It is one of the types of space resource depots that have been proposed for enabling infrastructure-based space exploration. Many different depot concepts exist depending on the type of fuel to be supplied, location, or type of depot which may also include a propellant tanker that delivers a single load to a spacecraft at a specified orbital location and then departs. In-space fuel depots are not necessarily located near or at a space station.

<span class="mw-page-title-main">Docking and berthing of spacecraft</span> Joining of two or more space vehicles

Docking and berthing of spacecraft is the joining of two space vehicles. This connection can be temporary, or partially permanent such as for space station modules.

<span class="mw-page-title-main">Space tug</span> Spacecraft used to transfer cargo from one orbit to another

A space tug is a type of spacecraft used to transfer spaceborne cargo from one orbit to another orbit with different energy characteristics. An example would be moving a spacecraft from a low Earth orbit (LEO) to a higher-energy orbit like a geostationary transfer orbit, a lunar transfer, or an escape trajectory.

The EELV Secondary Payload Adapter (ESPA) is an adapter for launching secondary payloads on orbital launch vehicles.

<span class="mw-page-title-main">Busek</span> American spacecraft propulsion company

Busek Co. Inc. is an American spacecraft propulsion company that builds thrusters, electronics, and various systems for spacecraft.

<span class="mw-page-title-main">Artemis 2</span> Artemis programs second lunar flight

Artemis 2 is the second scheduled mission of NASA's Artemis program and the first scheduled crewed mission of NASA's Orion spacecraft, currently planned to be launched by the Space Launch System (SLS) in November 2024. The crewed Orion spacecraft will perform a lunar flyby and return to Earth. Artemis 2 is planned to be the first crewed spacecraft to travel to the Moon, and beyond low Earth orbit, since Apollo 17 in 1972.

<span class="mw-page-title-main">Mars Cube One</span> 2018 Mars flyby mission

Mars Cube One was a Mars flyby mission launched on 5 May 2018 alongside NASA's InSight Mars lander. It consisted of two nanospacecraft, MarCO-A and MarCO-B, that provided real-time communications to Earth for InSight during its entry, descent, and landing (EDL) on 26 November 2018 - when InSight was out of line of sight from the Earth. Both spacecraft were 6U CubeSats designed to test miniaturized communications and navigation technologies. These were the first CubeSats to operate beyond Earth orbit, and aside from telecommunications they also tested CubeSats' endurance in deep space. On 5 February 2019, NASA reported that both the CubeSats had gone silent by 5 January 2019, and are unlikely to be heard from again. In August 2019, the CubeSats were honored for their role in the successful landing of the InSight lander on Mars.

<span class="mw-page-title-main">Lunar Flashlight</span> Lunar orbiter by NASA

Lunar Flashlight is a low-cost CubeSat lunar orbiter mission to explore, locate, and estimate size and composition of water ice deposits on the Moon for future exploitation by robots or humans.

<span class="mw-page-title-main">Lunar IceCube</span> Nanosatellite

Lunar IceCube is a NASA nanosatellite orbiter mission to prospect, locate, and estimate amount and composition of water ice deposits on the Moon for future exploitation by robots or humans. It was launched as a secondary payload mission on Artemis 1, the first flight of the Space Launch System (SLS), on 16 November 2022. As of February 2023 it's unknown whether NASA team has contact with satellite or not.

<span class="mw-page-title-main">LunIR</span> Spacecraft

LunIR is a nanosatellite spacecraft launched to the Moon collecting surface spectroscopy and thermography. It was launched as a secondary payload on the Artemis 1 mission on 16 November 2022.

<i>ArgoMoon</i> Nanosatellite

ArgoMoon is a CubeSat that was launched into a heliocentric orbit on Artemis 1, the maiden flight of the Space Launch System, on 16 November 2022 at 06:47:44 UTC. The objective of the ArgoMoon spacecraft is to take detailed images of the Interim Cryogenic Propulsion Stage following Orion separation, an operation that will demonstrate the ability of a cubesat to conduct precise proximity maneuvers in deep space.

Cislunar Explorers is a pair of spacecraft that will show the viability of water electrolysis propulsion and interplanetary optical navigation to orbit the Moon. Both spacecraft will launch mated together as two L-shaped 3U CubeSats, which fit together as a 6U CubeSat of about 10 cm × 20 cm × 30 cm.

<span class="mw-page-title-main">Earth Escape Explorer</span> US experimental communications satellite

Earth Escape Explorer (CU-E3) is a nanosatellite of the 6U CubeSat format that will demonstrate long-distance communications while in heliocentric orbit.

<span class="mw-page-title-main">EQUULEUS</span> Japanese nanosatellite

EQUULEUS is a nanosatellite of the 6U CubeSat format that will measure the distribution of plasma that surrounds the Earth (plasmasphere) to help scientists understand the radiation environment in that region. It will also demonstrate low-thrust trajectory control techniques, such as multiple lunar flybys, within the Earth-Moon region using water steam as propellant. The spacecraft was designed and developed jointly by the Japan Aerospace Exploration Agency (JAXA) and the University of Tokyo.

<span class="mw-page-title-main">OMOTENASHI</span> Small spacecraft and semi-hard lander of the 6U CubeSat format

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<span class="mw-page-title-main">CAPSTONE</span> NASA satellite to test the Lunar Gateway orbit

CAPSTONE is a lunar orbiter that will test and verify the calculated orbital stability planned for the Lunar Gateway space station. The spacecraft is a 12-unit CubeSat that will also test a navigation system that will measure its position relative to NASA's Lunar Reconnaissance Orbiter (LRO) without relying on ground stations. It was launched on 28 June 2022, arrived in lunar orbit on 14 November 2022, and was scheduled to orbit for six months. On 18 May 2023, it completed its primary mission to orbit in the near-rectilinear halo orbit for six months, but will stay on this orbit, continuing to perform experiments during an enhanced mission phase.

<span class="mw-page-title-main">Small Innovative Missions for Planetary Exploration</span> NASA program

Small Innovative Missions for Planetary Exploration (SIMPLEx) is a planetary exploration program operated by NASA. The program funds small, low-cost spacecraft for stand-alone planetary exploration missions. These spacecraft are intended to launch as secondary payloads on other missions and are riskier than Discovery or New Frontiers missions.

References

  1. "Cubist Movement". Space News. 2012-08-13. p. 30. When [the cubesat was invented] a little more than a decade ago, [it was] never imagined that the tiny satellites would be adopted by universities, companies and government agencies around the world. They simply wanted to design a spacecraft with capabilities similar to Sputnik that graduate student could design, build, test and operate. For size, the professors settled on a 10-centimeter cube because it was large enough to accommodate a basic communications payload, solar panels and a battery.
  2. 1 2 Woellert, Kirk; Ehrenfreund, Picco, Hertzfeld (15 February 2011). "Cubesats: Cost-effective science and technology platforms for emerging and developing nations" (PDF). Advances in Space Research. ISSN 0273-1177. 47 (4): 663. Bibcode:2011AdSpR..47..663W. doi:10.1016/j.asr.2010.10.009 . Retrieved 2014-02-28.{{cite journal}}: CS1 maint: multiple names: authors list (link)
  3. Yamanouchi, Kelly (2006-10-16). "Lunar challenge lures maverick". Denver Post. Retrieved 2014-02-28.
  4. "Summary: MICRO-SPACE INC., Dissolved December 22, 2011". Colorado Secretary of State. Retrieved 2014-06-27.
  5. "Micro-Space is Currently Manifested to fly two tiny CubeSats". Space Fellowship. 2010-05-29. Retrieved 2014-02-28.
  6. Teams striving to take dreams to the moon, Denver Post , 2007-10-28, accessed 2010-12-24.