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NASA signed a separate contract with Northrop for the fabrication of the HALO, and for integration with the Power and Propulsion Element (PPE), being built by Maxar, for US$935 million. [ 13 ] [ 14 ] In mid 2024, the module reached significant completion and entered into the stress test phase in Thales Alenia 's facilities.
The Lunar I-Hab [3] (formerly known as International Habitation Module, International Habitat or I-HAB) is designed as a habitat module of the Lunar Gateway station, to be built by the European Space Agency (ESA) in collaboration with the Japan Aerospace Exploration Agency, or JAXA.
Both PPE and HALO will be assembled on Earth and launched together on a Falcon Heavy rocket in 2027 [1] [44] They are expected to reach lunar orbit after nine to ten months. [45] The I-Hab module, a contribution from ESA and JAXA, is to be launched on the SLS Block 1B as a co-manifested payload on the Artemis IV crewed Orion mission. [ 46 ]
A Blue Origin New Shepard rocket lifts off from the company's launch site in West Texas on March 31, 2022. The mission carried five paying passengers and Gary Lai, New Shepard's chief architect ...
Rocket Flight number Launch site LSP; Payload (⚀ = CubeSat) Operator Orbit Function Decay (UTC) Outcome Remarks March (TBD) [1] SLS Block 1B Kennedy LC-39B: NASA: Artemis 5: NASA: Selenocentric Crewed lunar landing ESPRIT Refueling Module (ERM) ESA: Selenocentric Lunar Gateway component Lunar Terrain Vehicle: NASA: Selenocentric to lunar surface
It’s currently deployed on Navy Super Hornet jet and (soon) P-8 Poseidon patrol planes, as well as Air Force B-1Bs and even from a palletized launcher designed for release from C-130 and C-17 ...
In orbital mechanics a near-rectilinear halo orbit (NRHO) is a halo orbit that passes close to the smaller of two bodies and has nearly stable behavior. [1] The CAPSTONE mission, launched in 2022, is the first spacecraft to use such orbit in cislunar space, and this Moon-centric orbit is planned as a staging area for future lunar missions.
The PPE is intended to have a launch mass of 5,000 kg (11,000 lb) with propellant accounting for half that mass [1] and the capability to generate 50 kW [8] of solar electric power using Roll Out Solar Arrays for its Hall-effect thrusters, which can be supplemented by chemical propulsion. [9]