A thrust flow powered vehicle comprising: - a first thrust flow expeller (30, 130, 230, 330) for expelling a first thrust flow in a first direction, - a second thrust flow expeller (131, 231, 331) for expelling a second thrust flow in a second direction, the second direction being a different direction to the first direction but sharing a plane with the first direction, wherein the vehicle (10, 100, 200 or 300) further comprises: - a thrust flow outlet fairing (20, 120) associated with both the first and second thrust flow expellers, comprising: - a thrust flow deflector surface (24, 124) comprising a portion at an angle to the plane of the first and second directions, and - an outlet portion through which an output thrust flow is to be expelled, such that, in use, the thrust flow deflector surface deflects at least a portion of both the first and second thrust flows to form the output thrust flow such that the output thrust flow has a component in the plane of the first and second directions, and a component out of the plane of the first and second directions, the first thrust flow to be expelled by the first thrust flow expeller and the second thrust flow to be expelled by the second thrust flow expeller being independently controllable, and characterised in that the outlet fairing (20, 120) is substantially in the shape of a wedge, with a short angled portion (22, 122) towards one end and a tapered portion (21, 121) towards an opposite end and wherein the outlet portion is located on the short angled portion of the outlet fairing. - a first thrust flow expeller (30, 130, 230, 330) for expelling a first thrust flow in a first direction, - a second thrust flow expeller (131, 231, 331) for expelling a second thrust flow in a second direction, the second direction being a different direction to the first direction but sharing a plane with the first direction, - a thrust flow outlet fairing (20, 120) associated with both the first and second thrust flow expellers, comprising: - a thrust flow deflector surface (24, 124) comprising a portion at an angle to the plane of the first and second directions, and - an outlet portion through which an output thrust flow is to be expelled, such that, in use, the thrust flow deflector surface deflects at least a portion of both the first and second thrust flows to form the output thrust flow such that the output thrust flow has a component in the plane of the first and second directions, and a component out of the plane of the first and second directions, the first thrust flow to be expelled by the first thrust flow expeller and the second thrust flow to be expelled by the second thrust flow expeller being independently controllable, and characterised in that the outlet fairing (20, 120) is substantially in the shape of a wedge, with a short angled portion (22, 122) towards one end and a tapered portion (21, 121) towards an opposite end and wherein the outlet portion is located on the short angled portion of the outlet fairing. - a thrust flow deflector surface (24, 124) comprising a portion at an angle to the plane of the first and second directions, and - an outlet portion through which an output thrust flow is to be expelled,