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  2. EELV Secondary Payload Adapter - Wikipedia

    en.wikipedia.org/wiki/EELV_Secondary_Payload_Adapter

    The LDPE (Long Duration Propulsive ESPA) is based on a Northrop Grumman payload adapter used to help attach the upper stage to the main satellite in addition to hosting a few slots for other smallsats. However, the entire system is powered by the ESPAStar satellite bus, which is in charge of power consumption and distribution as well as ...

  3. Space tug - Wikipedia

    en.wikipedia.org/wiki/Space_tug

    2.2.3 Long Duration Propulsive ESPA (LDPE) 2.2.4 Vigoride by ... LDPE is based on a Northrop Grumman payload adapter used to help attach the upper stage to the ...

  4. List of Atlas launches (2020–2029) - Wikipedia

    en.wikipedia.org/wiki/List_of_Atlas_launches...

    Alongside STPSat-6 was an integrated propulsive EELV Secondary Payload Adapter (IP-ESPA) holding up to six payloads. [32] The STP-3 mission also debuted three engineering features designed to reduce risk and accumulate flight experience before use on Vulcan Centaur : an Out-of-Autoclave (OoA) payload fairings, an in-flight power system and GPS ...

  5. SHERPA (space tug) - Wikipedia

    en.wikipedia.org/wiki/SHERPA_(space_tug)

    SHERPA is a commercial satellite dispenser developed by Andrews Space, a subsidiary of Spaceflight Industries, [1] and was unveiled in 2012. The maiden flight was on 3 December 2018 on a Falcon 9 Block 5 rocket, and it consisted of two separate unpropelled variants of the dispenser.

  6. Orbital propellant depot - Wikipedia

    en.wikipedia.org/wiki/Orbital_propellant_depot

    It is one of the types of space resource depots that have been proposed for enabling infrastructure-based space exploration. [1] Many 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 ...

  7. Time loop thriller The Lazarus Project is propulsive drama - AOL

    www.aol.com/news/the-lazarus-project-review-time...

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  8. Rocket Lab Electron - Wikipedia

    en.wikipedia.org/wiki/Rocket_Lab_Electron

    There are nine Rutherford engines on the first stage and one vacuum-optimized version on the second stage. [26] [27] [28] The first stage engines deliver 162 kN (36,000 lb f) of thrust and the second stage delivers 22 kN (4,900 lb f) of thrust. Almost all of the engines' parts are 3D printed to save time and money in the manufacturing process ...

  9. Habitation and Logistics Outpost - Wikipedia

    en.wikipedia.org/wiki/Habitation_and_Logistics...

    Northrop offered a "minimal" 6.1-meter (20 feet) by 3-meter (9.8 feet) design based on the Cygnus spacecraft, as well as a larger 7-meter (22.9 feet) by 4.4-meter (14.4 feet) design also based on the Cygnus, [7] [12] to the outside of which radial docking ports, body-mounted radiators (BMRs), batteries and communications antennae will be added ...