User:Apogee7/sandbox
Comment: Fails WP:NCOMPANY - lacks any independent secondary sources or references. Potential WP:COI / WP:SELFPROMOTION. Dan arndt (talk) 01:57, 27 April 2022 (UTC)
Apogee Space
[edit]Apogee Spaceflight Incorporated (Known as Apogee Space) is a private aerospace manufacturer and space transportation company. Apogee Space was founded in December of 2021 with a goal of making the human species a multi-planetary species by establishing surface and orbital colonies on and around The Moon, Mars, and beyond.
Products
[edit]Launch Vehicles
[edit]Nautilus
[edit]The Nautilus is a heavy-lift, semi-reusable Falcon 9 Competitor currently under development. The rocket is equipped with 7 Hazel Atmos engines on the first stage, and 1 Hazel Vac engine on the upper stage. It is planned to launch a maximum of 10 tons to a Low Earth Orbit.
Nautilus Heavy
[edit]The Nautilus Heavy is an upgraded version of the Nautilus, Adding two boosters to each side of the first stage. The first stage with boosters uses 21 Hazel Atmos engines, and the same 1 Hazel Vac engine on the upper stage. It can launch a maximum of 30 tons to Low Earth Orbit.
Rocket Engines
[edit]Hazel Atmos
[edit]The Hazel Atmos is designed for the first stage of the Nautilus and Nautilus Heavy. It delivers 100,000 N of thrust at sea level. The engine is powered by Liquid Oxygen and Oxidizer. It is made of a heat-resistant titanium alloy.
Hazel Vac
[edit]The Hazel Vac is designed for the second stage of the Nautilus and Nautilus Heavy. it delivers 130,000 N of thrust in a vacuum. The engine is made of titanium alloy.
Hazel Mini
[edit]The Hazel Mini is a smaller version of the normal Hazel engines, at a small size of just 2ft tall. Hazel Mini is designed for the Phoenix Abort System and other landing systems. It delivers 50,000 N of thrust in a vacuum, and 40,000 N of thrust at sea-level.
Epsilon Atmos
[edit]Epsilon Atmos is a larger version of the Hazel Atmos engine designed for the Nautilus X. Thrust power is unknown.
Epsilon Vac
[edit]Epsilon Vac is a larger version of the Hazel Vac engine designed for the Nautilus X. Thrust power is unknown.
Human Launch/Transport/Landing Systems
[edit]Phoenix
[edit]![](http://upload.wikimedia.org/wikipedia/commons/thumb/1/16/Phoenix_Capsule_Render_-_Size_Reference.png/485px-Phoenix_Capsule_Render_-_Size_Reference.png)
Phoenix Capsule is a capsule designed for travel in the Earth-Moon System. The capsule replaces the cargo fairing on the Nautilus or Nautilus Heavy launch vehicle and sits on the Phoenix Service and Landing Module. The Capsule can carry 5 tons and 3 People to LEO, or 3 tons and 3 People to LLO.
Capsule Serial | Capsule Name | Total Capsule Flights | Capsule Status | Capsule Mission |
---|---|---|---|---|
PT001 | Phoenix Test 01 | 0 | Destroyed | Test Phoenix Capsule |
PT002 | Phoenix Test 02 | 0 | Retired | Test Phoenix Capsule |
PC1 | Glory | 0 | In Development | Conduct Spaceflight |
PC2 | Inspire | 0 | In Development | Conduct Spaceflight |
PC3 | Guardian | 0 | Concept Stage | Conduct Spaceflight |
PC4 | Horzions | 0 | Concept Stage | Conduct Spaceflight |
Phoenix X
[edit]Phoenix X is a bigger and more capable version of the standard Phoenix designed for travel to The Moon or Deep Space. The capsule replaces the cargo fairing on Nautilus or Nautilus Heavy and sits on the Phoenix Service and Landing Module.
Capsule Serial | Capsule Name | Total Capsule Flights | Capsule Status | Capsule Mission |
---|---|---|---|---|
PX001 | Phoenix X Test 01 | 0 | Concept Stage | Test Phoenix X |
PX002 | Phoenix X Test 02 | 0 | Concept Stage | Test Phoenix X |
PX1 | Beyond | 0 | Concept Stage | Conduct Spaceflight |
PX2 | Unity | 0 | Concept Stage | Conduct Spaceflight |
PX3 | Aurora | 0 | Concept Stage | Conduct Spaceflight |
PX4 | Pegasus | 0 | Concept Stage | Conduct Spaceflight |
Orbital Establishments
[edit]Helios Station
[edit]Helios Station is a space station planned to be established in LLO. The station will serve as the waypoint between Earth and The Moon, and eventually will be a pit-stop for ships flying interplanetary distances.