Neptune

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Neptune-30 [InterOrbital]

Neptune-45 [InterOrbital]

Neptune-1000 [InterOrbital]

InterOrbital Systems plans a series of small modular launch vehicles called Neptune consisting of clusters of simple pressure-fed rocket modules.

The IOS modular rocket system is an evolved version of a similar system developed by OTRAG in the 1970's. Lutz Kayser, the former head of the OTRAG team, is a primary consultant on the IOS project.

Each member of the Neptune Modular Series of launch vehicles is assembled from multiple Common Propulsion Modules (CPMs). Payload capacity can be varied by increasing or decreasing the number of CPMs. A single CPM will be flown as a test vehicle or as a sounding rocket.

Each Common Propulsion Module is composed of two tandem propellant tanks and a single throttleable, ablatively-cooled rocket engine. Depending on the configuration, the modules can operate in either blowdown or pressurant tank-fed modes. The capacity of the propellant tanks is regulated by varying their lengths. Construction costs are kept low by utilizing many off-the-shelf components. All CPM parts are interchangeable and mass-producible.

A single fixed, throttleable, low-thrust, liquid rocket engine powers each CPM. When the CPMs are clustered in multiples of three or four per stage, differential throttling of opposing rocket engines provides pitch, yaw and roll control. Stand-alone CPMs will be steered by four small gimbaled vernier rocket engines. Storable, high-density white fuming nitric acid (WFNA) and turpentine/furfuryl alcohol are the CPM’s primary propellants. These low-cost, storable, environmentally friendly propellants provide reliable, efficient, hypergolic ignition.

The Neptune-30 is a three stage (parallel staged) micro-satellite launch vehicle capable of launching 30-Kg payload into polar low-earth orbit. It is composed of 5 Common Propulsion Modules and a solid spin-stabilized satellite kick-stage. The engine count breaks down to 4 booster engines, 1 stage-2 engine, and 1 stage-3 engine (a total of 6 engines).

The Neptune-45 is a three stage (parallel staged) micro-satellite launch vehicle capable of launching 45-Kg payload into polar low-earth orbit. It is composed of 7 Common Propulsion Modules and a solid spin-stabilized or a liquid guided satellite kick-stage. The engine count breaks down to 6 booster engines, 1 stage two engine, and 1 stage three motor or engine (a total of 8 engines).

The Neptune-1000 is a four stage (parallel staged), medium-lift launch vehicle capable of placing a 1000-Kg payload into polar low-earth orbit or accelerating a 190-Kg payload to Earth-escape velocity. The rocket is composed of 33 Common Propulsion Modules. The engine count breaks down to 24 booster engines, 6 stage two engines, 2 stage three engines, and 1 stage four engine.

Flights of the CPM and the Neptune series have been announced for several years to be imminent, without any visible progress happening.

No:   TNo: Serial    Type              Date          LS            Payload

none
 

* = suborbital