Mars Outpost Demo [NanoRacks]
The Mars Outpost Demo is an experiment with the overall goal, to demonstrate metal cutting in space and to explore the feasibility of reusing abandoned space vehicles.
The experiment will be launched on the second stage of a SpaceX Falcon 9 launch vehicle on a dedicated sun-sync rideshare mission. The experiment remains attached to the second stage throughout the mission and during de-orbit. Stage 2 will be inserted into a circular orbit at about 545 km, 97.5 degrees inclination. Transmission and experiment initiation will be enabled by the Stage 2 on board computer after deployment of satellite payloads from Stage 2. This is estimated to be about 45 minutes after second stage engine cutoff. After completion of the mission, Stage 2 will be deorbited.
The payload system is a cutting experiment. A video camera will record a high speed cutting wheel cutting a coupon of CRES 316 stainless steel. The experiment will demonstrate cutting characteristics in zero g and vacuum.
|Type / Application:||Technology|
|Configuration:||Experiment bolted to Falcon upper stage|
|Mass:||111 kg (experiment only)|
|Mars Outpost Demo||2022-002||13.01.2022||CC SLC-40||Falcon-9 v1.2 (Block 5)||with Umbra 02, Capella 7, 8, ICEYE X14, X16, Sich 2-1, ION-SCV 004, Dodona, STORK 1, 2, LabSat, SW1FT, VZLUSAT 2, ETV A1, BRO 5, HYPSO 1, Kepler 16, ..., 19, OroraTech 1, Flock-4x 1, ..., 44, Lemur-2 146, ..., 149, DEWA-Sat 1, NuX 1, IRIS A, MDASat 1a, 1b, 1c, Gossamer Piccolomini, Tevel 1, ..., 8, Challenger, Delfi-PQ 1, Unicorn 2A, 2D, 2E, FossaSat 2E1, ..., 2E6, MDQube-SAT 1, SATTLA 2A, 2B, Unicorn 1, EASAT 2, HADES, Grizu-263a, PION-BR 1, SanoSat 1, Tartan-Artibeus 1, Mars Outpost Demo|